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 22829U 93061G 23338.13468794 .00000233 00000-0 10519-3 0 9990
2 22829 98.7963 24.1396 0009069 222.4710 137.5772 14.31367569575749
| Epoch (UTC): | 04 December 2023 03:13:57 |
| Eccentricity: | 0.0009069 |
| inclination: | 98.7963° |
| perigee height: | 780 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 24.1396° |
| argument of perigee: | 222.4710° |
| revolutions per day: | 14.31367569 |
| mean anomaly at epoch: | 137.5772° |
| orbit number at epoch: | 57574 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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