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 62250U 26145.59443654 +.00000000 +00000-0 +14069-3 0 00009
2 62250 89.0100 24.7679 0016218 81.4446 278.8542 13.51007974 08
| Epoch (UTC): | 25 May 2026 14:15:59 |
| Eccentricity: | 0.0016218 |
| inclination: | 89.0100° |
| perigee height: | 1056 km |
| apogee height: | 1081 km |
| right ascension of ascending node: | 24.7679° |
| argument of perigee: | 81.4446° |
| revolutions per day: | 13.51007974 |
| mean anomaly at epoch: | 278.8542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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