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 62501U 26145.46419036 +.00000000 +00000-0 +44343-3 0 00009
2 62501 43.0006 215.3497 0001443 276.3905 83.6782 15.27595718 08
| Epoch (UTC): | 25 May 2026 11:08:26 |
| Eccentricity: | 0.0001443 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 215.3497° |
| argument of perigee: | 276.3905° |
| revolutions per day: | 15.27595718 |
| mean anomaly at epoch: | 83.6782° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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