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 23154.64050683 .00001993 00000-0 20292-3 0 9991
2 22286 82.5183 118.8046 0022397 86.8910 273.4871 14.90071182646362
| Epoch (UTC): | 03 June 2023 15:22:19 |
| Eccentricity: | 0.0022397 |
| inclination: | 82.5183° |
| perigee height: | 582 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 118.8046° |
| argument of perigee: | 86.8910° |
| revolutions per day: | 14.90071182 |
| mean anomaly at epoch: | 273.4871° |
| orbit number at epoch: | 64636 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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