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 is defined by the following mean orbital elements,
1 22825U 26145.41440539 +.00000000 +00000-0 +47324-4 0 00004
2 22825 98.6888 212.8351 0008799 160.1409 200.0117 14.30935115 07
| Epoch (UTC): | 25 May 2026 09:56:44 |
| Eccentricity: | 0.0008799 |
| inclination: | 98.6888° |
| perigee height: | 782 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 212.8351° |
| argument of perigee: | 160.1409° |
| revolutions per day: | 14.30935115 |
| mean anomaly at epoch: | 200.0117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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