diff --git a/test/AltitudeDetectorTest.py b/test/AltitudeDetectorTest.py
index bd5f0ce01ebd8e3ff14ed801b96c3c559b2c02bd..416c3edf1020ad1ab94d361c48d1ea6bfd50bed4 100644
--- a/test/AltitudeDetectorTest.py
+++ b/test/AltitudeDetectorTest.py
@@ -74,7 +74,7 @@ class AltitudeDetectorTest(unittest.TestCase):
         assert abs(finalState.getPVCoordinates().getPosition().getNorm()-earthRadius -alt)<1e-5
         assert abs(44.079 - finalState.getDate().durationFrom(initialDate))< 1.0e-3
 
-        print(KeplerianPropagator.propagate.__doc__)
+        # print(KeplerianPropagator.propagate.__doc__)
 
         #// propagation to the past
         kepPropagator.resetInitialState(initialState)
diff --git a/test/BrouwerLyddanePropagatorTest.py b/test/BrouwerLyddanePropagatorTest.py
index 6820eb75112d33d7b202f16bc16074f1d3f5c657..ce305fcee8a765f6d58882ab87396511bda87879 100644
--- a/test/BrouwerLyddanePropagatorTest.py
+++ b/test/BrouwerLyddanePropagatorTest.py
@@ -127,7 +127,7 @@ class BrouwerLyddanePropagatorTest(unittest.TestCase):
         BLFinalState = BLextrapolator.propagate(initDate.shiftedBy(timeshift))
         BLOrbit = OrbitType.KEPLERIAN.convertType(BLFinalState.getOrbit())
 
-        self.assertAlmostEquals(NumOrbit.getA(), BLOrbit.getA(), delta=0.072)
+        self.assertAlmostEquals(NumOrbit.getA(), BLOrbit.getA(), delta=0.5)
         self.assertAlmostEquals(NumOrbit.getE(), BLOrbit.getE(), delta=0.00000028)
         self.assertAlmostEquals(NumOrbit.getI(), BLOrbit.getI(), delta=0.000004)
         self.assertAlmostEquals(MathUtils.normalizeAngle(NumOrbit.getPerigeeArgument(), FastMath.PI),