View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 31944U 99025CMV 24353.12246666 .00003059 00000-0 15698-2 0 9994
2 31944 99.1647 126.3631 0154411 290.6677 245.1667 14.10203266907927
| Epoch (UTC): | 18 December 2024 02:56:21 |
| Eccentricity: | 0.0154411 |
| inclination: | 99.1647° |
| perigee height: | 747 km |
| apogee height: | 970 km |
| right ascension of ascending node: | 126.3631° |
| argument of perigee: | 290.6677° |
| revolutions per day: | 14.10203266 |
| mean anomaly at epoch: | 245.1667° |
| orbit number at epoch: | 90792 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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