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 00107U 61013A 22279.82450315 .00002675 00000-0 33564-3 0 9993
2 00107 28.7905 106.1333 0540652 240.8955 113.6445 14.10494505 85036
| Epoch (UTC): | 06 October 2022 19:47:17 |
| Eccentricity: | 0.0540652 |
| inclination: | 28.7905° |
| perigee height: | 466 km |
| apogee height: | 1249 km |
| right ascension of ascending node: | 106.1333° |
| argument of perigee: | 240.8955° |
| revolutions per day: | 14.10494505 |
| mean anomaly at epoch: | 113.6445° |
| orbit number at epoch: | 8503 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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