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 24357.67883638 .00000273 00000-0 12185-3 0 9990
2 22825 98.7638 52.1886 0007464 244.4047 115.6364 14.30686149629564
| Epoch (UTC): | 22 December 2024 16:17:31 |
| Eccentricity: | 0.0007464 |
| inclination: | 98.7638° |
| perigee height: | 784 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 52.1886° |
| argument of perigee: | 244.4047° |
| revolutions per day: | 14.30686149 |
| mean anomaly at epoch: | 115.6364° |
| orbit number at epoch: | 62956 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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