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 22825U 93061C 23086.08035900 .00000275 00000-0 12388-3 0 9991
2 22825 98.8524 127.6060 0007552 312.6229 47.4315 14.30271996538825
| Epoch (UTC): | 27 March 2023 01:55:43 |
| Eccentricity: | 0.0007552 |
| inclination: | 98.8524° |
| perigee height: | 785 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 127.6060° |
| argument of perigee: | 312.6229° |
| revolutions per day: | 14.30271996 |
| mean anomaly at epoch: | 47.4315° |
| orbit number at epoch: | 53882 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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