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 107U 61013A 23336.03994391 .00005184 00000-0 65852-3 0 9991
2 107 28.7856 236.1315 0527490 151.8606 211.1544 14.13737778144163
| Epoch (UTC): | 02 December 2023 00:57:31 |
| Eccentricity: | 0.0527490 |
| inclination: | 28.7856° |
| perigee height: | 465 km |
| apogee height: | 1228 km |
| right ascension of ascending node: | 236.1315° |
| argument of perigee: | 151.8606° |
| revolutions per day: | 14.13737778 |
| mean anomaly at epoch: | 211.1544° |
| orbit number at epoch: | 14416 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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