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 55962U 26145.48967190 +.00000000 +00000-0 +24946-4 0 00001
2 55962 70.0004 70.9508 0002792 270.5409 89.5430 14.98331786 05
| Epoch (UTC): | 25 May 2026 11:45:07 |
| Eccentricity: | 0.0002792 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 70.9508° |
| argument of perigee: | 270.5409° |
| revolutions per day: | 14.98331786 |
| mean anomaly at epoch: | 89.5430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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