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 40057U 14034E 23339.81962322 .00004212 00000-0 51696-3 0 9990
2 40057 98.3581 180.7437 0010612 53.2010 307.0175 14.83632511508867
| Epoch (UTC): | 05 December 2023 19:40:15 |
| Eccentricity: | 0.0010612 |
| inclination: | 98.3581° |
| perigee height: | 610 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 180.7437° |
| argument of perigee: | 53.2010° |
| revolutions per day: | 14.83632511 |
| mean anomaly at epoch: | 307.0175° |
| orbit number at epoch: | 50886 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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