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 57882U 26145.52495778 +.00000000 +00000-0 +62081-4 0 00009
2 57882 42.9989 211.6799 0001405 271.1740 88.8951 15.27578922 07
| Epoch (UTC): | 25 May 2026 12:35:56 |
| Eccentricity: | 0.0001405 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.6799° |
| argument of perigee: | 271.1740° |
| revolutions per day: | 15.27578922 |
| mean anomaly at epoch: | 88.8951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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