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Copy of PropagatorBuilder
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4
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81
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April 18, 2024
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Setting AemMetadata's Reference Frame
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2
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60
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April 18, 2024
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Conversion of TLE
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8
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4339
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April 18, 2024
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Distance/range event detector
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4
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72
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April 17, 2024
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Spacecraft orbital tube monitoring
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12
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166
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April 17, 2024
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Default method `build()` in `PropagatorBuilder`?
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4
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56
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April 16, 2024
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Mass rate in SpacecraftState
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2
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61
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April 15, 2024
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Antex reader, problem with getSatelliteAntennas method
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1
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45
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April 15, 2024
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Doppler shift using Orekit
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13
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105
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April 13, 2024
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Attitude not applied inside handlers (Orekit 12)
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4
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80
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April 12, 2024
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Updates for High Fidelity Heliocentric Propagation
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12
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1027
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April 12, 2024
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Get local orbital frame
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1
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59
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April 11, 2024
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BooleanDetector.andCombine() short circuit evaluation
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1
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63
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April 11, 2024
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Propagation With NRLMSISE00 force model throw Exception after upgrade to orekit 12.0
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6
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219
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April 11, 2024
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use `DateDetector` to retrieve the state of an orbit within a specific time sequence, but it is not working
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2
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53
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April 11, 2024
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Default position angle in NumericalPropagator
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15
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341
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April 10, 2024
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Revamping AdditionalStateProvider or adding a method to Propagator
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8
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100
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April 10, 2024
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Integration history
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4
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68
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April 10, 2024
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Eckstein Hechler propagator Initial orbit behavior
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1
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44
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April 9, 2024
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Drag Area changing Control during Propagation
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1
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104
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April 9, 2024
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Loading the GRGM1200B lunar gravity model
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5
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43
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April 9, 2024
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Hipparchus version for Orekit develop branch
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2
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49
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April 8, 2024
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NaN appears during the integration
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10
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206
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April 8, 2024
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CelestialBodyPointing to Earth center and perfect circular KeplerianOrbit
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2
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73
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April 6, 2024
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JavaStackTrace Error when calling WMM Model
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1
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43
|
April 6, 2024
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Hipparchus 3.1 released
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3
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76
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April 6, 2024
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STM propagation
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5
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91
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April 5, 2024
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[VOTE] Releasing hipparchus 3.1 from release candidate 2
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5
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69
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April 5, 2024
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InvalidArgError for 'org.orekit.models.earth.GeoMagneticField'
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6
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71
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April 4, 2024
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Get initial guess using finite differencing from measurements
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5
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130
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April 4, 2024
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