| generateKeplerianOrbit() |   | 74% | | 50% | 1 | 2 | 1 | 6 | 0 | 1 |
| generateTLE() | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| OMMFile() | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| generateSpacecraftState() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setTLERelatedParametersComment(List) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| generateCartesianOrbit() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setbStar(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setMeanMotionDot(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setMeanMotionDotDot(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setMeanMotion(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setEphemerisType(int) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setClassificationType(char) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setNoradID(Integer) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setElementSetNo(String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setRevAtEpoch(int) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getBStar() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMeanMotionDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMeanMotionDotDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getTLERelatedParametersComment() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMetaData() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMeanMotion() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEphemerisType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getClassificationType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getNoradID() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getElementSetNumber() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getRevAtEpoch() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |