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 22888U 93070A 23341.62389535 .00000056 00000-0 42835-4 0 9998
2 22888 82.9525 43.9810 0047007 241.0108 273.1993 13.75032154507232
| Epoch (UTC): | 07 December 2023 14:58:24 |
| Eccentricity: | 0.0047007 |
| inclination: | 82.9525° |
| perigee height: | 947 km |
| apogee height: | 1016 km |
| right ascension of ascending node: | 43.9810° |
| argument of perigee: | 241.0108° |
| revolutions per day: | 13.75032154 |
| mean anomaly at epoch: | 273.1993° |
| orbit number at epoch: | 50723 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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