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 65846U 26145.58335647 +.00000000 +00000-0 +15980-3 0 00007
2 65846 53.1587 90.9766 0001055 96.3542 95.0314 15.33578790 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001055 |
| inclination: | 53.1587° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 90.9766° |
| argument of perigee: | 96.3542° |
| revolutions per day: | 15.33578790 |
| mean anomaly at epoch: | 95.0314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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