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 23079.85423479 .00000198 00000-0 94119-4 0 9997
2 22825 98.8535 121.2717 0007824 332.4480 27.6286 14.30267723537668
| Epoch (UTC): | 20 March 2023 20:30:05 |
| Eccentricity: | 0.0007824 |
| inclination: | 98.8535° |
| perigee height: | 785 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 121.2717° |
| argument of perigee: | 332.4480° |
| revolutions per day: | 14.30267723 |
| mean anomaly at epoch: | 27.6286° |
| orbit number at epoch: | 53766 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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