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 23029.73380659 .00004607 00000-0 59204-3 0 9996
2 00107 28.7886 175.3427 0537598 214.9645 141.4471 14.11229033101275
| Epoch (UTC): | 29 January 2023 17:36:40 |
| Eccentricity: | 0.0537598 |
| inclination: | 28.7886° |
| perigee height: | 466 km |
| apogee height: | 1244 km |
| right ascension of ascending node: | 175.3427° |
| argument of perigee: | 214.9645° |
| revolutions per day: | 14.11229033 |
| mean anomaly at epoch: | 141.4471° |
| orbit number at epoch: | 10127 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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