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 57885U 26145.46842032 +.00000000 +00000-0 +63388-4 0 00005
2 57885 42.9999 211.2603 0001366 272.1612 87.9084 15.27577705 01
| Epoch (UTC): | 25 May 2026 11:14:31 |
| Eccentricity: | 0.0001366 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.2603° |
| argument of perigee: | 272.1612° |
| revolutions per day: | 15.27577705 |
| mean anomaly at epoch: | 87.9084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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