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 23893U 96029A 22297.65721194 0.00000000 00000-0 00000-0 0 01
2 23893 63.3113 163.3626 3398152 268.6168 91.3832 5.52856044 04
| Epoch (UTC): | 24 October 2022 15:46:23 |
| Eccentricity: | 0.3398152 |
| inclination: | 63.3113° |
| perigee height: | 2541 km |
| apogee height: | 11723 km |
| right ascension of ascending node: | 163.3626° |
| argument of perigee: | 268.6168° |
| revolutions per day: | 5.52856044 |
| mean anomaly at epoch: | 91.3832° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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