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 22286U 92094A 24276.72100496 .00010830 00000-0 10275-2 0 9993
2 22286 82.5229 16.7188 0018232 259.5165 100.4001 14.93326003697896
| Epoch (UTC): | 02 October 2024 17:18:14 |
| Eccentricity: | 0.0018232 |
| inclination: | 82.5229° |
| perigee height: | 575 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 16.7188° |
| argument of perigee: | 259.5165° |
| revolutions per day: | 14.93326003 |
| mean anomaly at epoch: | 100.4001° |
| orbit number at epoch: | 69789 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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