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 62251U 26145.61911275 +.00000000 +00000-0 +14131-3 0 00002
2 62251 89.0105 24.7824 0017870 82.5965 277.7216 13.51004701 00
| Epoch (UTC): | 25 May 2026 14:51:31 |
| Eccentricity: | 0.0017870 |
| inclination: | 89.0105° |
| perigee height: | 1055 km |
| apogee height: | 1082 km |
| right ascension of ascending node: | 24.7824° |
| argument of perigee: | 82.5965° |
| revolutions per day: | 13.51004701 |
| mean anomaly at epoch: | 277.7216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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