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 62244U 26145.66025545 +.00000000 +00000-0 +16149-3 0 00006
2 62244 89.0103 24.7927 0017523 82.5996 277.7146 13.51005707 02
| Epoch (UTC): | 25 May 2026 15:50:46 |
| Eccentricity: | 0.0017523 |
| inclination: | 89.0103° |
| perigee height: | 1056 km |
| apogee height: | 1082 km |
| right ascension of ascending node: | 24.7927° |
| argument of perigee: | 82.5996° |
| revolutions per day: | 13.51005707 |
| mean anomaly at epoch: | 277.7146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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