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 02389U 66070A 22275.83236829 .00006661 00000-0 36252-3 0 9990
2 02389 81.3881 42.7140 1199302 312.1402 38.3642 13.01688783419992
| Epoch (UTC): | 02 October 2022 19:58:36 |
| Eccentricity: | 0.1199302 |
| inclination: | 81.3881° |
| perigee height: | 340 km |
| apogee height: | 2171 km |
| right ascension of ascending node: | 42.7140° |
| argument of perigee: | 312.1402° |
| revolutions per day: | 13.01688783 |
| mean anomaly at epoch: | 38.3642° |
| orbit number at epoch: | 41999 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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