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 24282.42562821 .00001766 00000-0 69341-3 0 9992
2 22825 98.7754 336.3163 0009427 106.4275 253.7944 14.30614578618809
| Epoch (UTC): | 08 October 2024 10:12:54 |
| Eccentricity: | 0.0009427 |
| inclination: | 98.7754° |
| perigee height: | 783 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 336.3163° |
| argument of perigee: | 106.4275° |
| revolutions per day: | 14.30614578 |
| mean anomaly at epoch: | 253.7944° |
| orbit number at epoch: | 61880 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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