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 25201.40682479 .00000061 00000-0 40523-4 0 9993
2 22825 98.7345 263.1616 0008290 1.5158 358.6048 14.30810104659557
| Epoch (UTC): | 20 July 2025 09:45:49 |
| Eccentricity: | 0.0008290 |
| inclination: | 98.7345° |
| perigee height: | 783 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 263.1616° |
| argument of perigee: | 1.5158° |
| revolutions per day: | 14.30810104 |
| mean anomaly at epoch: | 358.6048° |
| orbit number at epoch: | 65955 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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