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 22175.49522007 .00000875 00000-0 98584-4 0 9993
2 00107 28.7898 336.5725 0542214 4.5917 355.9381 14.10110581 70291
| Epoch (UTC): | 24 June 2022 11:53:07 |
| Eccentricity: | 0.0542214 |
| inclination: | 28.7898° |
| perigee height: | 466 km |
| apogee height: | 1251 km |
| right ascension of ascending node: | 336.5725° |
| argument of perigee: | 4.5917° |
| revolutions per day: | 14.10110581 |
| mean anomaly at epoch: | 355.9381° |
| orbit number at epoch: | 7029 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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