OrekitMessages_en.utf8 35.8 KB
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# internal error, please notify development team by creating a new topic at {0}
INTERNAL_ERROR = internal error, please notify development team by creating a new topic at {0}
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# altitude ({0} m) is below the {1} m allowed threshold
ALTITUDE_BELOW_ALLOWED_THRESHOLD = altitude ({0} m) is below the {1} m allowed threshold

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# point is inside ellipsoid
POINT_INSIDE_ELLIPSOID = point is inside ellipsoid

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# trajectory inside the Brillouin sphere (r = {0})
TRAJECTORY_INSIDE_BRILLOUIN_SPHERE = trajectory inside the Brillouin sphere (r = {0})

# almost equatorial orbit (i = {0} degrees)
ALMOST_EQUATORIAL_ORBIT = almost equatorial orbit (i = {0} degrees)

# almost critically inclined orbit (i = {0} degrees)
ALMOST_CRITICALLY_INCLINED_ORBIT = almost critically inclined orbit (i = {0} degrees)

# unable to compute Eckstein-Hechler mean parameters after {0} iterations
UNABLE_TO_COMPUTE_ECKSTEIN_HECHLER_MEAN_PARAMETERS = unable to compute Eckstein-Hechler mean parameters after {0} iterations

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# unable to compute Brouwer-Lyddane mean parameters after {0} iterations
UNABLE_TO_COMPUTE_BROUWER_LYDDANE_MEAN_PARAMETERS = unable to compute Brouwer-Lyddane mean parameters after {0} iterations

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# unable to compute TLE after {0} iterations
UNABLE_TO_COMPUTE_TLE = unable to compute TLE after {0} iterations

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# null parent for frame {0}
NULL_PARENT_FOR_FRAME = null parent for frame {0}

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# frame {0} is already attached to frame {1}
FRAME_ALREADY_ATTACHED = frame {0} is already attached to frame {1}

# frame {0} is not attached to the main frames tree
FRAME_NOT_ATTACHED = frame {0} is not attached to the main frames tree

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# frame {0} is an ancestor of both frames {1} and {2}
FRAME_ANCESTOR_OF_BOTH_FRAMES = frame {0} is an ancestor of both frames {1} and {2}

# frame {0} is an ancestor of neither frame {1} nor {2}
FRAME_ANCESTOR_OF_NEITHER_FRAME = frame {0} is an ancestor of neither frame {1} nor {2}

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# frame {0} has depth {1}, it cannot have an ancestor {2} levels above
FRAME_NO_NTH_ANCESTOR = frame {0} has depth {1}, it cannot have an ancestor {2} levels above

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# ITRF frame {0} not found
NO_SUCH_ITRF_FRAME = ITRF frame {0} not found
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# unsupported local orbital frame {0}
UNSUPPORTED_LOCAL_ORBITAL_FRAME = unsupported local orbital frame {0}
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# non pseudo-inertial frame "{0}"
NON_PSEUDO_INERTIAL_FRAME = non pseudo-inertial frame "{0}"
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# data root directory {0} does not exist
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DATA_ROOT_DIRECTORY_DOES_NOT_EXIST = data root directory {0} does not exist
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# {0} is not a directory
NOT_A_DIRECTORY = {0} is not a directory

# {0} is neither a directory nor a zip/jar archive file
NEITHER_DIRECTORY_NOR_ZIP_OR_JAR = {0} is neither a directory nor a zip/jar archive file

# unable to find resource {0} in classpath
UNABLE_TO_FIND_RESOURCE = unable to find resource {0} in classpath

# no Earth Orientation Parameters loaded
NO_EARTH_ORIENTATION_PARAMETERS_LOADED = no Earth Orientation Parameters loaded

# missing Earth Orientation Parameters between {0} and {1}
MISSING_EARTH_ORIENTATION_PARAMETERS_BETWEEN_DATES = missing Earth Orientation Parameters between {0} and {1}

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# missing Earth Orientation Parameters between {0} and {1}, gap is {2,number,0.0##############E0} s
MISSING_EARTH_ORIENTATION_PARAMETERS_BETWEEN_DATES_GAP = missing Earth Orientation Parameters between {0} and {1}, gap is {2,number,0.0##############E0} s

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# missing Earth Orientation Parameters
NO_EARTH_ORIENTATION_PARAMETERS = missing Earth Orientation Parameters

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# file {0} is not a supported IERS data file
NOT_A_SUPPORTED_IERS_DATA_FILE = file {0} is not a supported IERS data file

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# inconsistent dates in IERS file {0}: {1}-{2}-{3} and MJD {4}
INCONSISTENT_DATES_IN_IERS_FILE = inconsistent dates in IERS file {0}: {1}-{2}-{3} and MJD {4}

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# unexpected data after line {0} in file {1}: {2}
UNEXPECTED_DATA_AFTER_LINE_IN_FILE = unexpected data after line {0} in file {1}: {2}

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# unexpected data at line {0} in file {1}
UNEXPECTED_DATA_AT_LINE_IN_FILE = unexpected data at line {0} in file {1}

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# non-chronological dates in file {0}, line {1}
NON_CHRONOLOGICAL_DATES_IN_FILE = non-chronological dates in file {0}, line {1}

# no IERS UTC-TAI history data loaded
NO_IERS_UTC_TAI_HISTORY_DATA_LOADED = no IERS UTC-TAI history data loaded

# no entries found in IERS UTC-TAI history file {0}
NO_ENTRIES_IN_IERS_UTC_TAI_HISTORY_FILE =  no entries found in IERS UTC-TAI history file {0}

# missing serie j = {0} in file {1} (line {2})
MISSING_SERIE_J_IN_FILE = missing serie j = {0} in file {1} (line {2})

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# cannot parse both τ and γ from the same Poissons series file
CANNOT_PARSE_BOTH_TAU_AND_GAMMA = cannot parse both τ and γ from the same Poissons series file

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# unexpected end of file {0} (after line {1})
UNEXPECTED_END_OF_FILE_AFTER_LINE = unexpected end of file {0} (after line {1})

# unable to parse line {0} of file {1}:\n{2}
UNABLE_TO_PARSE_LINE_IN_FILE = unable to parse line {0} of file {1}:\n{2}

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# unable to parse element {0} at line {1}, file {2}
UNABLE_TO_PARSE_ELEMENT_IN_FILE = <MISSING TRANSLATION>

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# unable to find file {0}
UNABLE_TO_FIND_FILE = unable to find file {0}

# spacecraft mass becomes negative: {0} kg
SPACECRAFT_MASS_BECOMES_NEGATIVE = spacecraft mass becomes negative: {0} kg

# positive flow rate (q: {0})
POSITIVE_FLOW_RATE = positive flow rate (q: {0})

# no gravity field data loaded
NO_GRAVITY_FIELD_DATA_LOADED = no gravity field data loaded

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# gravity field normalization underflow for degree {0} and order {1}
GRAVITY_FIELD_NORMALIZATION_UNDERFLOW  = gravity field normalization underflow for degree {0} and order {1}

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# no ocean tide data loaded
NO_OCEAN_TIDE_DATA_LOADED = no ocean tide data loaded

# ocean tide data file {0} limited to degree {1} and order {2}
OCEAN_TIDE_DATA_DEGREE_ORDER_LIMITS = ocean tide data file {0} limited to degree {1} and order {2}

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# load deformation coefficients limited to degree {0}, cannot parse degree {1} term from file {2}
OCEAN_TIDE_LOAD_DEFORMATION_LIMITS = load deformation coefficients limited to degree {0}, cannot parse degree {1} term from file {2}

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# polar trajectory (distance to polar axis: {0})
POLAR_TRAJECTORY = polar trajectory (distance to polar axis: {0})

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# unexpected format error for file {0} with loader {1}
UNEXPECTED_FILE_FORMAT_ERROR_FOR_LOADER = unexpected format error for file {0} with loader {1}
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# duplicated gravity field coefficient {0}({1}, {2}) in file {3}
DUPLICATED_GRAVITY_FIELD_COEFFICIENT_IN_FILE = duplicated gravity field coefficient {0}({1}, {2}) in file {3}

# missing gravity field coefficient {0}({1}, {2}) in file {3}
MISSING_GRAVITY_FIELD_COEFFICIENT_IN_FILE = missing gravity field coefficient {0}({1}, {2}) in file {3}

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# too large degree (n = {0}, potential maximal degree is {1})
TOO_LARGE_DEGREE_FOR_GRAVITY_FIELD = too large degree (n = {0}, potential maximal degree is {1})

# too large order (m = {0}, potential maximal order is {1})
TOO_LARGE_ORDER_FOR_GRAVITY_FIELD = too large order (m = {0}, potential maximal order is {1})

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# several reference dates ({0} and {1} differ by {3,number,0.0##############E0} s) found in gravity field file {2}
SEVERAL_REFERENCE_DATES_IN_GRAVITY_FIELD = several reference dates ({0} and {1} differ by {3,number,0.0##############E0} s) found in gravity field file {2}
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# no TLE data available for object {0}
NO_TLE_FOR_OBJECT = no TLE data available for object {0}

# no TLE data available for launch year {0}, launch number {1}, launch piece {2}
NO_TLE_FOR_LAUNCH_YEAR_NUMBER_PIECE = no TLE data available for launch year {0}, launch number {1}, launch piece {2}

# lines {0} and {1} are not TLE lines:\n{0}: "{2}"\n{1}: "{3}"
NOT_TLE_LINES = lines {0} and {1} are not TLE lines:\n{0}: "{2}"\n{1}: "{3}"

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# expected a second TLE line after line {0}:\n{0}: "{1}"
MISSING_SECOND_TLE_LINE = expected a second TLE line after line {0}:\n{0}: "{1}"
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# TLE lines do not refer to the same object:\n{0}\n{1}
TLE_LINES_DO_NOT_REFER_TO_SAME_OBJECT = TLE lines do not refer to the same object:\n{0}\n{1}

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# invalid TLE parameter for object {0}: {1} = {2}
TLE_INVALID_PARAMETER = invalid TLE parameter for object {0}: {1} = {2}

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# wrong checksum of TLE line {0}, expected {1} but got {2} ({3})
TLE_CHECKSUM_ERROR = wrong checksum of TLE line {0}, expected {1} but got {2} ({3})

# no TLE data available
NO_TLE_DATA_AVAILABLE = no TLE data available

# spacecraft mass is not positive: {0} kg
NOT_POSITIVE_SPACECRAFT_MASS = spacecraft mass is not positive: {0} kg

# too large eccentricity for propagation model: e = {0}
TOO_LARGE_ECCENTRICITY_FOR_PROPAGATION_MODEL = too large eccentricity for propagation model: e = {0}

# no solar activity available at {0}, data available only in range [{1}, {2}]
NO_SOLAR_ACTIVITY_AT_DATE = no solar activity available at {0}, data available only in range [{1}, {2}]

# non-existent month {0}
NON_EXISTENT_MONTH = non-existent month {0}

# non-existent date {0}-{1}-{2}
NON_EXISTENT_YEAR_MONTH_DAY = non-existent date {0}-{1}-{2}

# non-existent week date {0}-W{1}-{2}
NON_EXISTENT_WEEK_DATE = non-existent week date {0}-W{1}-{2}

# non-existent date {0}
NON_EXISTENT_DATE = non-existent date {0}

# no day number {0} in year {1}
NON_EXISTENT_DAY_NUMBER_IN_YEAR = no day number {0} in year {1}

# non-existent time {0}:{1}:{2}
NON_EXISTENT_HMS_TIME = non-existent time {0}:{1}:{2}

# non-existent time {0}
NON_EXISTENT_TIME = non-existent time {0}

# out of range seconds number: {0}
OUT_OF_RANGE_SECONDS_NUMBER = out of range seconds number: {0}

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# out of range seconds number: {0} is not in [{1}, {2}]
OUT_OF_RANGE_SECONDS_NUMBER_DETAIL = out of range seconds number: {0} is not in [{1}, {2}]
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# angle type not supported, supported angles: {0}, {1} and {2}
ANGLE_TYPE_NOT_SUPPORTED = angle type not supported, supported angles: {0}, {1} and {2}

# satellite collided with target
SATELLITE_COLLIDED_WITH_TARGET = satellite collided with target

# attitude pointing law misses ground
ATTITUDE_POINTING_LAW_DOES_NOT_POINT_TO_GROUND = attitude pointing law misses ground

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# {0} seconds transition time for attitudes switch is too short, should be longer than {1} seconds
TOO_SHORT_TRANSITION_TIME_FOR_ATTITUDES_SWITCH = {0} seconds transition time for attitudes switch is too short, should be longer than {1} seconds

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# orbit date ({0}) does not match attitude date ({1})
ORBIT_AND_ATTITUDE_DATES_MISMATCH = orbit date ({0}) does not match attitude date ({1})

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# frame ({0}) does not match frame ({1})
FRAMES_MISMATCH = frame {0} does not match frame {1}
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# initial state not specified for orbit propagation
INITIAL_STATE_NOT_SPECIFIED_FOR_ORBIT_PROPAGATION = initial state not specified for orbit propagation

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# target event date must be before {1} by {3,number,0.0##############E0} seconds or after {2} by {3,number,0.0##############E0} seconds, but target event date {0} is {4,number,0.0##############E0} seconds before {1} and {5,number,0.0##############E0} seconds after {2} so it cannot be added
EVENT_DATE_TOO_CLOSE = target event date must be before {1} by {3,number,0.0##############E0} seconds or after {2} by {3,number,0.0##############E0} seconds, but target event date {0} is {4,number,0.0##############E0} seconds before {1} and {5,number,0.0##############E0} seconds after {2} so it cannot be added
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# unable to read header record from JPL ephemerides binary file {0}
UNABLE_TO_READ_JPL_HEADER = unable to read header record from JPL ephemerides binary file {0}

# inconsistent values of astronomical unit in JPL ephemerides files: ({0} and {1})
INCONSISTENT_ASTRONOMICAL_UNIT_IN_FILES = inconsistent values of astronomical unit in JPL ephemerides files: ({0} and {1})

# inconsistent values of Earth/Moon mass ratio in JPL ephemerides files: ({0} and {1})
INCONSISTENT_EARTH_MOON_RATIO_IN_FILES = inconsistent values of Earth/Moon mass ratio in JPL ephemerides files: ({0} and {1})

# no data loaded for celestial body {0}
NO_DATA_LOADED_FOR_CELESTIAL_BODY = no data loaded for celestial body {0}

# file {0} is not a JPL ephemerides binary file
NOT_A_JPL_EPHEMERIDES_BINARY_FILE = file {0} is not a JPL ephemerides binary file

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# file {0} is not a Marshall Solar Activity Future Estimation (MSAFE) file
NOT_A_MARSHALL_SOLAR_ACTIVITY_FUTURE_ESTIMATION_FILE = file {0} is not a Marshall Solar Activity Future Estimation (MSAFE) file

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# no JPL ephemerides binary files found
NO_JPL_EPHEMERIDES_BINARY_FILES_FOUND = no JPL ephemerides binary files found

# out of range date for {0} ephemerides: {1}
OUT_OF_RANGE_BODY_EPHEMERIDES_DATE = out of range date for {0} ephemerides: {1}

# out of range date for ephemerides: {0}, [{1}, {2}]
OUT_OF_RANGE_EPHEMERIDES_DATE = out of range date for ephemerides: {0}, [{1}, {2}]

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# out of range date for ephemerides: {0} is {3,number,0.0##############E0} s before [{1}, {2}]
OUT_OF_RANGE_EPHEMERIDES_DATE_BEFORE = out of range date for ephemerides: {0} is {3,number,0.0##############E0} s before [{1}, {2}]

# out of range date for ephemerides: {0} is {3,number,0.0##############E0} s after [{1}, {2}]
OUT_OF_RANGE_EPHEMERIDES_DATE_AFTER = out of range date for ephemerides: {0} is {3,number,0.0##############E0} s after [{1}, {2}]

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# unexpected two elevation values: {0} and {1}, for one azimuth: {2}
UNEXPECTED_TWO_ELEVATION_VALUES_FOR_ONE_AZIMUTH = unexpected two elevation values: {0} and {1}, for one azimuth: {2}

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# unsupported parameter name {0}, supported names: {1}
UNSUPPORTED_PARAMETER_NAME = unsupported parameter name {0}, supported names: {1}
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# scale factor for parameter {0} is too small: {1}
TOO_SMALL_SCALE_FOR_PARAMETER = scale factor for parameter {0} is too small: {1}
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# unknown additional state "{0}"
UNKNOWN_ADDITIONAL_STATE = unknown additional state "{0}"
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# unknown month "{0}"
UNKNOWN_MONTH = unknown month "{0}"

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# Jacobian matrix for type {0} is singular with current orbit
SINGULAR_JACOBIAN_FOR_ORBIT_TYPE = Jacobian matrix for type {0} is singular with current orbit

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# state Jacobian has not been initialized yet
STATE_JACOBIAN_NOT_INITIALIZED = state Jacobian has not been initialized yet
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# state Jacobian is a {0}x{1} matrix, it should be a 6x6 matrix
STATE_JACOBIAN_NOT_6X6 = state Jacobian is a {0}x{1} matrix, it should be a 6x6 matrix
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# state Jacobian has {0} rows but parameters Jacobian has {1} rows
STATE_AND_PARAMETERS_JACOBIANS_ROWS_MISMATCH = state Jacobian has {0} rows but parameters Jacobian has {1} rows
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# initial Jacobian matrix has {0} columns, but {1} parameters have been selected
INITIAL_MATRIX_AND_PARAMETERS_NUMBER_MISMATCH = initial Jacobian matrix has {0} columns, but {1} parameters have been selected
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# orbit should be either elliptic with a > 0 and e < 1 or hyperbolic with a < 0 and e > 1, a = {0}, e = {1}
ORBIT_A_E_MISMATCH_WITH_CONIC_TYPE = orbit should be either elliptic with a > 0 and e < 1 or hyperbolic with a < 0 and e > 1, a = {0}, e = {1}

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# true anomaly {0} out of hyperbolic range (e = {1}, {2} < v < {3})
ORBIT_ANOMALY_OUT_OF_HYPERBOLIC_RANGE = true anomaly {0} out of hyperbolic range (e = {1}, {2} < v < {3})

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# hyperbolic orbits cannot be handled as {0} instances
HYPERBOLIC_ORBIT_NOT_HANDLED_AS = hyperbolic orbits cannot be handled as {0} instances

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# invalid preamble field in CCSDS date: {0}
CCSDS_DATE_INVALID_PREAMBLE_FIELD = invalid preamble field in CCSDS date: {0}

# invalid time field length in CCSDS date: {0}, expected {1}
CCSDS_DATE_INVALID_LENGTH_TIME_FIELD = invalid time field length in CCSDS date: {0}, expected {1}

# missing agency epoch in CCSDS date
CCSDS_DATE_MISSING_AGENCY_EPOCH = missing agency epoch in CCSDS date
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# missing mandatory key {0} in CCSDS file {1}
CCSDS_MISSING_KEYWORD = missing mandatory key {0} in CCSDS file {1}

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# key {0} is not allowed in format version {1}
CCSDS_KEYWORD_NOT_ALLOWED_IN_VERSION = key {0} is not allowed in format version {1}

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# unexpected keyword in CCSDS line number {0} of file {1}:\n{2}
CCSDS_UNEXPECTED_KEYWORD = unexpected keyword in CCSDS line number {0} of file {1}:\n{2}
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# the central body gravitational coefficient cannot be retrieved from the ODM
CCSDS_UNKNOWN_GM = the central body gravitational coefficient cannot be retrieved from the ODM
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# there is no spacecraft mass associated with this ODM file
CCSDS_UNKNOWN_SPACECRAFT_MASS = there is no spacecraft mass associated with this ODM file

# no IERS conventions have been set before parsing
CCSDS_UNKNOWN_CONVENTIONS = no IERS conventions have been set before parsing

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# frame {0} is not valid in this CCSDS file context
CCSDS_INVALID_FRAME = frame {0} is not valid in this CCSDS file context
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# inconsistent time systems: {0} ≠ {1}
CCSDS_INCONSISTENT_TIME_SYSTEMS = inconsistent time systems: {0} ≠ {1}
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# No CCSDS TDM keyword was found at line {0} of file {1}:\n{2}
CCSDS_TDM_KEYWORD_NOT_FOUND = No CCSDS TDM keyword was found at line {0} of file {1}:\n{2}

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# no Range Units converter configured for parsing Tracking Data Message
CCSDS_TDM_MISSING_RANGE_UNITS_CONVERTER = no Range Units converter configured for parsing Tracking Data Message
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# Time system should have already been set before line {0} of file {1}
CCSDS_TIME_SYSTEM_NOT_READ_YET = Time system should have already been set before line {0} of file {1}
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# name "{0}" is already used for an additional state
ADDITIONAL_STATE_NAME_ALREADY_IN_USE = name "{0}" is already used for an additional state
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# reset state not allowed
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NON_RESETABLE_STATE = reset state not allowed
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# Cannot compute Newcomb operators for sigma > rho ({0} > {1})
DSST_NEWCOMB_OPERATORS_COMPUTATION = Cannot compute Newcomb operators for sigma > rho ({0} > {1})

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# Cannot compute the Vmns coefficient with m > n ({0} > {1})
DSST_VMNS_COEFFICIENT_ERROR_MS = Cannot compute the Vmns coefficient with m > n ({0} > {1})
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# inconsistent shadow computation: entry = {0} whereas exit = {1}
DSST_SPR_SHADOW_INCONSISTENT = inconsistent shadow computation: entry = {0} whereas exit = {1}

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# The current orbit has an eccentricity ({0} > 0.5). DSST needs an unimplemented time dependent numerical method to compute the averaged rates
DSST_ECC_NO_NUMERICAL_AVERAGING_METHOD = The current orbit has an eccentricity ({0} > 0.5). DSST needs an unimplemented time dependent numerical method to compute the averaged rates

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# unsupported sp3 file version {0}
SP3_UNSUPPORTED_VERSION = unsupported sp3 file version {0}
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# found {0} epochs in file {1}, expected {2}
SP3_NUMBER_OF_EPOCH_MISMATCH = found {0} epochs in file {1}, expected {2}

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# unexpected end of file in sp3 file (after line {0})
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SP3_UNEXPECTED_END_OF_FILE = unexpected end of sp3 file (after line {0})
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# unsupported clock file version {0}
CLOCK_FILE_UNSUPPORTED_VERSION = unsupported clock file version {0}
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# unsupported navigation messages file version {0}
NAVIGATION_FILE_UNSUPPORTED_VERSION = unsupported navigation messages file version {0}

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# non-existent geomagnetic model {0} for year {1}
NON_EXISTENT_GEOMAGNETIC_MODEL = non-existent geomagnetic model {0} for year {1}
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# geomagnetic model {0} with epoch {1} does not support time transformation, no secular variation coefficients defined
UNSUPPORTED_TIME_TRANSFORM = geomagnetic model {0} with epoch {1} does not support time transformation, no secular variation coefficients defined

# time transformation of geomagnetic model {0} with epoch {1} is outside its validity range: {2} != [{3}, {4}]
OUT_OF_RANGE_TIME_TRANSFORM = time transformation of geomagnetic model {0} with epoch {1} is outside its validity range: {2} != [{3}, {4}]
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# not enough data for interpolation (sample size = {0})
NOT_ENOUGH_DATA_FOR_INTERPOLATION = not enough data for interpolation (sample size = {0})

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# too small number of cached neighbors: {0} (must be at least {1})
NOT_ENOUGH_CACHED_NEIGHBORS =  too small number of cached neighbors: {0} (must be at least {1})
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# no cached entries
NO_CACHED_ENTRIES = no cached entries
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# generated entries not sorted: {0} > {1} by {2,number,0.0##############E0} s
NON_CHRONOLOGICALLY_SORTED_ENTRIES = generated entries not sorted: {0} > {1} by {2,number,0.0##############E0} s
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# no data generated around date: {0}
NO_DATA_GENERATED = no data generated around date: {0}
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# unable to generate new data before {0}, but data is requested for {1} which is {2,number,0.0##############E0} s before
UNABLE_TO_GENERATE_NEW_DATA_BEFORE = unable to generate new data before {0}, but data is requested for {1} which is {2,number,0.0##############E0} s before
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# unable to generate new data after {0}, but data is requested for {1} which is {2,number,0.0##############E0} s after then
UNABLE_TO_GENERATE_NEW_DATA_AFTER = unable to generate new data after {0}, but data is requested for {1} which is {2,number,0.0##############E0} s after
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# unable to compute hyperbolic eccentric anomaly from the mean anomaly after {0} iterations
UNABLE_TO_COMPUTE_HYPERBOLIC_ECCENTRIC_ANOMALY = unable to compute hyperbolic eccentric anomaly from the mean anomaly after {0} iterations
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# unable to compute mean orbit from osculating orbit after {0} iterations
UNABLE_TO_COMPUTE_DSST_MEAN_PARAMETERS = unable to compute mean orbit from osculating orbit after {0} iterations
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# derivation order {0} is out of range
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OUT_OF_RANGE_DERIVATION_ORDER = derivation order {0} is out of range
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# orbit type {0} not allowed here, allowed types: {1}
ORBIT_TYPE_NOT_ALLOWED = orbit type {0} not allowed here, allowed types: {1}
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# non pseudo-inertial frame {0} is not suitable as reference for inertial forces
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NON_PSEUDO_INERTIAL_FRAME_NOT_SUITABLE_AS_REFERENCE_FOR_INERTIAL_FORCES = non pseudo-inertial frame {0} is not suitable as reference for inertial forces
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# method not available in the absence of a central body
METHOD_NOT_AVAILABLE_WITHOUT_CENTRAL_BODY = method not available in the absence of a central body

# operation not available between frames {0} and {1}
INCOMPATIBLE_FRAMES = operation not available between frames {0} and {1}

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# orbit not defined, state rather contains an absolute position-velocity-acceleration
UNDEFINED_ORBIT = orbit not defined, state rather contains an absolute position-velocity-acceleration
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# absolute position-velocity-acceleration not defined, state rather contains an orbit
UNDEFINED_ABSOLUTE_PVCOORDINATES = absolute position-velocity-acceleration not defined, state rather contains an orbit
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# an inertial force model has to be used when propagating in non-inertial frame {0}
INERTIAL_FORCE_MODEL_MISSING = an inertial force model has to be used when propagating in non-inertial frame {0}
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# no SEM almanac file found
NO_SEM_ALMANAC_AVAILABLE = no SEM almanac file found

# file {0} is not a supported SEM almanac file
NOT_A_SUPPORTED_SEM_ALMANAC_FILE = file {0} is not a supported SEM almanac file

# no Yuma almanac file found
NO_YUMA_ALMANAC_AVAILABLE = no Yuma almanac file found

# file {0} is not a supported Yuma almanac file
NOT_A_SUPPORTED_YUMA_ALMANAC_FILE = file {0} is not a supported Yuma almanac file

# only {0} GNSS orbits are provided while {1} are needed to compute the DOP
NOT_ENOUGH_GNSS_FOR_DOP = only {0} GNSS orbits are provided while {1} are needed to compute the DOP
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# use of time system {0} in CCSDS files requires an additional ICD and is not implemented in Orekit
CCSDS_TIME_SYSTEM_NOT_IMPLEMENTED = use of time system {0} in CCSDS files requires an additional ICD and is not implemented in Orekit
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# inconsistent time systems in the attitude blocks: {0} ≠ {1}
CCSDS_AEM_INCONSISTENT_TIME_SYSTEMS = inconsistent time systems in the attitude blocks: {0} ≠ {1}

# attitude type {0} in CCSDS AEM files is not implemented in Orekit
CCSDS_AEM_ATTITUDE_TYPE_NOT_IMPLEMENTED = attitude type {0} in CCSDS AEM files is not implemented in Orekit

# invalid rotation sequence {0} at line {1} of file {2}
CCSDS_INVALID_ROTATION_SEQUENCE = <MISSING TRANSLATION>

# element set type {0} ({1}) is not supported yet
CCSDS_UNSUPPORTED_ELEMENT_SET_TYPE = element set type {0} ({1}) is not supported yet

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# retrograde factor not supported in element set {0}
CCSDS_UNSUPPORTED_RETROGRADE_EQUINOCTIAL = retrograde factor not supported in element set {0}

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# element set type {0} ({1}) expects {2} elements
CCSDS_ELEMENT_SET_WRONG_NB_COMPONENTS = element set type {0} ({1}) expects {2} elements

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# wrong number of units for maneuver {0}
CCSDS_MANEUVER_UNITS_WRONG_NB_COMPONENTS = wrong number of units for maneuver {0}

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# missing time field for maneuver {0}
CCSDS_MANEUVER_MISSING_TIME = missing time field for maneuver {0}

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# Creating an aggregate propagator requires at least one constituent propagator, but none were provided.
NOT_ENOUGH_PROPAGATORS = Creating an aggregate propagator requires at least one constituent propagator, but none were provided.
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# Creating an aggregate attitude provider requires at least one constituent attitude provider, but none were provided.
NOT_ENOUGH_ATTITUDE_PROVIDERS = Creating an aggregate attitude provider requires at least one constituent attitude provider, but none were provided.
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# argument {0} cannot be null
NULL_ARGUMENT = argument {0} cannot be null

# value {0} not found in {1}
VALUE_NOT_FOUND = value {0} not found in {1}

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# Klobuchar coefficients α or β could not be loaded from {0}
KLOBUCHAR_ALPHA_BETA_NOT_LOADED = Klobuchar coefficients α or β could not be loaded from {0}

# Klobuchar coefficients α or β not available for date {0}
KLOBUCHAR_ALPHA_BETA_NOT_AVAILABLE_FOR_DATE = Klobuchar coefficients α or β not available for date {0}

# file {0} does not contain Klobuchar coefficients α or β
NO_KLOBUCHAR_ALPHA_BETA_IN_FILE = file {0} does not contain Klobuchar coefficients α or β
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# no reference date set for parameter {0}
NO_REFERENCE_DATE_FOR_PARAMETER = no reference date set for parameter {0}
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# station {0} not found, known stations: {1}
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STATION_NOT_FOUND = station {0} not found, known stations: {1}
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# unknown satellite system {0}
UNKNOWN_SATELLITE_SYSTEM = unknown satellite system {0}

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# unknown time system {0}
UNKNOWN_TIME_SYSTEM = unknown time system {0}

# unknown clock data type {0}
UNKNOWN_CLOCK_DATA_TYPE = unknown clock data type {0}

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# unknown satellite antenna code {0}
UNKNOWN_SATELLITE_ANTENNA_CODE = unknown satellite antenna code {0}

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# frequency {0} is not supported by antenna {1}
UNSUPPORTED_FREQUENCY_FOR_ANTENNA = frequency {0} is not supported by antenna {1}

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# cannot find satellite {0} in satellite system {1}
CANNOT_FIND_SATELLITE_IN_SYSTEM = cannot find satellite {0} in satellite system {1}

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# unknown RINEX frequency {0} in file {1}, line {2}
UNKNOWN_RINEX_FREQUENCY = unknown RINEX frequency {0} in file {1}, line {2}

# mismatched frequencies in file {0}, line {1} (expected {2}, got {3})
MISMATCHED_FREQUENCIES = mismatched frequencies in file {0}, line {1} (expected {2}, got {3})
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# wrong number of columns in file {0}, line {1} (expected {2} columns, got {3} columns)
WRONG_COLUMNS_NUMBER = wrong number of columns in file {0}, line {1} (expected {2} columns, got {3} columns)

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# unsupported format for file {0}
UNSUPPORTED_FILE_FORMAT = unsupported format for file {0}
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# incomplete header in file {0}
INCOMPLETE_HEADER = incomplete header in file {0}

# inconsistent number of satellites in line {0}, file {1}: observation with {2} satellites and number of max satellites is {3}
INCONSISTENT_NUMBER_OF_SATS = inconsistent number of satellites in line {0}, file {1}: observation with {2} satellites and number of max satellites is {3}

# the satellite system {3} from line {0}, file {1} is not consistent with the Rinex Satellite System {2} in header
INCONSISTENT_SATELLITE_SYSTEM = the satellite system {3} from line {0}, file {1} is not consistent with the Rinex Satellite System {2} in header
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# no propagator configured
NO_PROPAGATOR_CONFIGURED = no propagator configured

# dimension {0} is inconsistent with parameters list: {1}
DIMENSION_INCONSISTENT_WITH_PARAMETERS = dimension {0} is inconsistent with parameters list: {1}
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# file {0} is not a supported Unix-compressed file
NOT_A_SUPPORTED_UNIX_COMPRESSED_FILE = file {0} is not a supported Unix-compressed file

# unexpected end of file {0}
UNEXPECTED_END_OF_FILE = unexpected end of file {0}

# file {0} is corrupted
CORRUPTED_FILE = file {0} is corrupted
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# Vienna coefficients ah or aw or zh or zw could not be loaded from {0}
VIENNA_ACOEF_OR_ZENITH_DELAY_NOT_LOADED = Vienna coefficients ah or aw or zh or zw could not be loaded from {0}
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# Vienna coefficients ah or aw or zh or zw not available for date {0}
VIENNA_ACOEF_OR_ZENITH_DELAY_NOT_AVAILABLE_FOR_DATE = Vienna coefficients ah or aw or zh or zw not available for date {0}
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# file {0} does not contain Vienna coefficients ah, aw, zh or zw
NO_VIENNA_ACOEF_OR_ZENITH_DELAY_IN_FILE = file {0} does not contain Vienna coefficients ah, aw, zh or zw
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# irregular or incomplete grid in file {0}
IRREGULAR_OR_INCOMPLETE_GRID = irregular or incomplete grid in file {0}
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# invalid satellite system {0}
INVALID_SATELLITE_SYSTEM = invalid satellite system {0}
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# IONEX file {0} does not contain TEC data for date {1}
NO_TEC_DATA_IN_FILE_FOR_DATE = IONEX file {0} does not contain TEC data for date {1}

# number of maps {0} is inconsistent with header specification: {1}
INCONSISTENT_NUMBER_OF_TEC_MAPS_IN_FILE = number of maps {0} is inconsistent with header specification: {1}
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# file {0} does not contain latitude or longitude bondaries in its header section
NO_LATITUDE_LONGITUDE_BONDARIES_IN_IONEX_HEADER = file {0} does not contain latitude or longitude bondaries in its header section

# file {0} does not contain epoch of first or last map in its header section
NO_EPOCH_IN_IONEX_HEADER = file {0} does not contain epoch of first or last map in its header section

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# The first column of itrf-versions.conf is a plain prefix that is matched against the
# name of each loaded file. It should not contain any regular expression syntax or
# directory components, i.e. \"/\" or \"\\\". Actual value: \"{0}\".
ITRF_VERSIONS_PREFIX_ONLY = The first column of itrf-versions.conf is a plain prefix that is matched against the name of each loaded file. It should not contain any regular expression syntax or directory components, i.e. "/" or "\\". Actual value: "{0}".
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# cannot compute aiming direction at singular point: latitude = {0}, longitude = {1}
CANNOT_COMPUTE_AIMING_AT_SINGULAR_POINT = cannot compute aiming direction at singular point: latitude = {0}, longitude = {1}
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# STEC integration did not converge
STEC_INTEGRATION_DID_NOT_CONVERGE = STEC integration did not converge

# MODIP grid not be loaded from {0}
MODIP_GRID_NOT_LOADED = MODIP grid not be loaded from {0}

# NeQuick coefficient f2 or fm3 not be loaded from {0}
NEQUICK_F2_FM3_NOT_LOADED = NeQuick coefficient f2 or fm3 not be loaded from {0}
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# file {0} is not a supported Hatanaka-compressed file
NOT_A_SUPPORTED_HATANAKA_COMPRESSED_FILE = file {0} is not a supported Hatanaka-compressed file
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# Cannot compute around {0}
CANNOT_COMPUTE_LAGRANGIAN = Cannot compute around {0}

# The trajectory does not cross XZ Plane, it will not result in a Halo Orbit
TRAJECTORY_NOT_CROSSING_XZPLANE = The trajectory does not cross XZ Plane, it will not result in a Halo Orbit
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# The multiple shooting problem is underconstrained : {0} free variables, {1} constraints
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MULTIPLE_SHOOTING_UNDERCONSTRAINED = The multiple shooting problem is underconstrained : {0} free variables, {1} constraints

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# invalid measurement types {0} and {1} for the combination of measurements {2}
INVALID_MEASUREMENT_TYPES_FOR_COMBINATION_OF_MEASUREMENTS = invalid measurement types {0} and {1} for the combination of measurements {2}
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# frequencies {0} and {1} are incompatibles for the {2} combination
INCOMPATIBLE_FREQUENCIES_FOR_COMBINATION_OF_MEASUREMENTS = frequencies {0} and {1} are incompatibles for the {2} combination
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# observations are not in chronological order: {0} is {2,number,0.0##############E0} s after {1}
NON_CHRONOLOGICAL_DATES_FOR_OBSERVATIONS = observations are not in chronological order: {0} is {2,number,0.0##############E0} s after {1}
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# Use of the ExceptionalDataContext detected. This is typically used to detect developer errors.
EXCEPTIONAL_DATA_CONTEXT = Use of the ExceptionalDataContext detected. This is typically used to detect developer errors.

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# Observations must have different dates: {0}, {1} ({3,number,0.0##############E0} s from first observation), and {2} ({4,number,0.0##############E0} s from first observation, {5,number,0.0##############E0} s from second observation)
NON_DIFFERENT_DATES_FOR_OBSERVATIONS = Observations must have different dates: {0}, {1} ({3,number,0.0##############E0} s from first observation), and {2} ({4,number,0.0##############E0} s from first observation, {5,number,0.0##############E0} s from second observation)
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# observations are not in the same plane
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NON_COPLANAR_POINTS = observations are not in the same plane
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# invalid parameter {0}: {1} not in range [{2}, {3}]
INVALID_PARAMETER_RANGE = invalid parameter {0}: {1} not in range [{2}, {3}]
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# The parameter {0} should not be null in {1}
PARAMETER_NOT_SET = The parameter {0} should not be null in {1}

# {0} is not implemented
FUNCTION_NOT_IMPLEMENTED = {0} is not implemented

# Impossible to execute {0} with {1} set to {2}
INVALID_TYPE_FOR_FUNCTION = Impossible to execute {0} with {1} set to {2}
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# No data could be parsed from file {0}
NO_DATA_IN_FILE = No data could be parsed from file {0}
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# Unexpected end of CPF file (after line {0})
CPF_UNEXPECTED_END_OF_FILE = Unexpected end of CPF file (after line {0})

# Unexpected file format. Must be {0} but is {1}
UNEXPECTED_FORMAT_FOR_ILRS_FILE = Unexpected file format. Must be {0} but is {1}
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# Invalid range indicator {0} in CRD file header
INVALID_RANGE_INDICATOR_IN_CRD_FILE = Invalid range indicator {0} in CRD file header

# Unexpected end of CRD file (after line {0})
CRD_UNEXPECTED_END_OF_FILE = Unexpected end of CRD file (after line {0})
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# end of encoded message reached
END_OF_ENCODED_MESSAGE = end of encoded message reached

# too large data type ({0} bits)
TOO_LARGE_DATA_TYPE = too large data type ({0} bits)

# unknown encoded message number {0}
UNKNOWN_ENCODED_MESSAGE_NUMBER = unknown encoded message number {0}
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# unknown authentication method: {0}
UNKNOWN_AUTHENTICATION_METHOD = unknown authentication method: {0}

# unknown carrier phase code: {0}
UNKNOWN_CARRIER_PHASE_CODE = unknown carrier phase code: {0}

# unknown data format: {0}
UNKNOWN_DATA_FORMAT = unknown data format: {0}

# unknown navigation system: {0}
UNKNOWN_NAVIGATION_SYSTEM = unknown navigation system: {0}

# data stream {0} requires a NMEA fix data
STREAM_REQUIRES_NMEA_FIX = data stream {0} requires a NMEA fix data

# failed authentication for mountpoint {0}
FAILED_AUTHENTICATION = failed authentication for mountpoint {0}

# error connecting to {0}: {1}
CONNECTION_ERROR = error connecting to {0}: {1}

# unexpected content type {0}
UNEXPECTED_CONTENT_TYPE = unexpected content type {0}

# cannot parse GNSS data from {0}
CANNOT_PARSE_GNSS_DATA = cannot parse GNSS data from {0}

# unknown host {0}
UNKNOWN_HOST = unknown host {0}

# error parsing sourcetable line {0} from {1}: {2}
SOURCETABLE_PARSE_ERROR = error parsing sourcetable line {0} from {1}: {2}

# cannot parse sourcetable from {0}
CANNOT_PARSE_SOURCETABLE = cannot parse sourcetable from {0}

# mount point {0} is already connected
MOUNPOINT_ALREADY_CONNECTED = mount point {0} is already connected

# missing header from {0}: {1}
MISSING_HEADER = missing header from {0}: {1}
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# {0} is not a valid international designator
NOT_VALID_INTERNATIONAL_DESIGNATOR = {0} is not a valid international designator
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# value for key {0} has not been initialized
UNINITIALIZED_VALUE_FOR_KEY = value for key {0} has not been initialized
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# unknown unit {0}
UNKNOWN_UNIT = unknown unit {0}

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# units {0} and {1} are not compatible
INCOMPATIBLE_UNITS = units {0} and {1} are not compatible

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# missing velocity data
MISSING_VELOCITY = missing velocity data
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# attempt to generate file {0} with a formatting error
ATTEMPT_TO_GENERATE_MALFORMED_FILE = attempt to generate file {0} with a formatting error
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# {0} failed to find root between {1} (g={2,number,0.0##############E0}) and {3} (g={4,number,0.0##############E0})\nLast iteration at {5} (g={6,number,0.0##############E0})
FIND_ROOT = {0} failed to find root between {1} (g={2,number,0.0##############E0}) and {3} (g={4,number,0.0##############E0})\nLast iteration at {5} (g={6,number,0.0##############E0})
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# backward propagation not allowed here
BACKWARD_PROPAGATION_NOT_ALLOWED = backward propagation not allowed here
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# no station eccentricity values for the given epoch {0}, validity interval is between {1} and {2}
NO_STATION_ECCENTRICITY_FOR_EPOCH = no station eccentricity values for the given epoch {0}, validity interval is between {1} and {2}
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# inconsistent parameters selection between pairs {0}/{1} and {2}/{3}
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INCONSISTENT_SELECTION = <MISSING TRANSLATION>