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 24256.40760271 .00000674 00000-0 27582-3 0 9998
2 22825 98.7800 310.0602 0008513 176.7164 183.4075 14.30578231615086
| Epoch (UTC): | 12 September 2024 09:46:56 |
| Eccentricity: | 0.0008513 |
| inclination: | 98.7800° |
| perigee height: | 784 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 310.0602° |
| argument of perigee: | 176.7164° |
| revolutions per day: | 14.30578231 |
| mean anomaly at epoch: | 183.4075° |
| orbit number at epoch: | 61508 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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