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 31793U 07029B 24357.53852413 -.00000021 00000-0 14008-4 0 9994
2 31793 70.9767 21.7502 0003066 277.5415 194.3581 14.14728327902836
| Epoch (UTC): | 22 December 2024 12:55:28 |
| Eccentricity: | 0.0003066 |
| inclination: | 70.9767° |
| perigee height: | 841 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 21.7502° |
| argument of perigee: | 277.5415° |
| revolutions per day: | 14.14728327 |
| mean anomaly at epoch: | 194.3581° |
| orbit number at epoch: | 90283 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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