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ORbit Extrapolation KIT
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EphemerisFile.EphemerisSegment
EphemerisFile.EphemerisSegment
Element
Missed Instructions
Cov.
Missed Branches
Cov.
Missed
Cxty
Missed
Lines
Missed
Methods
Total
0 of 15
100%
0 of 2
100%
0
3
0
5
0
2
getInertialFrame()
100%
100%
0
2
0
4
0
1
getPropagator()
100%
n/a
0
1
0
1
0
1