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 23268.37769803 .00006974 00000-0 89700-3 0 9996
2 00107 28.7905 260.8964 0531058 248.6774 105.6320 14.12833256135030
| Epoch (UTC): | 25 September 2023 09:03:53 |
| Eccentricity: | 0.0531058 |
| inclination: | 28.7905° |
| perigee height: | 466 km |
| apogee height: | 1233 km |
| right ascension of ascending node: | 260.8964° |
| argument of perigee: | 248.6774° |
| revolutions per day: | 14.12833256 |
| mean anomaly at epoch: | 105.6320° |
| orbit number at epoch: | 13503 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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