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 29093U 06015B 22140.50435649 .00036904 00000-0 48249-3 0 9992
2 29093 97.6045 358.1808 0038695 286.7527 72.9483 15.57635845895304
| Epoch (UTC): | 20 May 2022 12:06:16 |
| Eccentricity: | 0.0038695 |
| inclination: | 97.6045° |
| perigee height: | 368 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 358.1808° |
| argument of perigee: | 286.7527° |
| revolutions per day: | 15.57635845 |
| mean anomaly at epoch: | 72.9483° |
| orbit number at epoch: | 89530 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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