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 24281.44647149 .00000830 00000-0 33513-3 0 9993
2 22825 98.7755 335.3285 0009429 109.0915 251.1289 14.30606267618930
| Epoch (UTC): | 07 October 2024 10:42:55 |
| Eccentricity: | 0.0009429 |
| inclination: | 98.7755° |
| perigee height: | 783 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 335.3285° |
| argument of perigee: | 109.0915° |
| revolutions per day: | 14.30606267 |
| mean anomaly at epoch: | 251.1289° |
| orbit number at epoch: | 61893 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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