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 23150.50459941 .00003879 00000-0 49136-3 0 9990
2 00107 28.7900 210.3401 0533807 244.4321 110.0147 14.12147885118356
| Epoch (UTC): | 30 May 2023 12:06:37 |
| Eccentricity: | 0.0533807 |
| inclination: | 28.7900° |
| perigee height: | 466 km |
| apogee height: | 1238 km |
| right ascension of ascending node: | 210.3401° |
| argument of perigee: | 244.4321° |
| revolutions per day: | 14.12147885 |
| mean anomaly at epoch: | 110.0147° |
| orbit number at epoch: | 11835 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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