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 57893U 26145.31741105 +.00000000 +00000-0 +38081-3 0 00008
2 57893 43.0013 241.5493 0001288 279.8984 80.1722 15.27584508 04
| Epoch (UTC): | 25 May 2026 07:37:04 |
| Eccentricity: | 0.0001288 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 241.5493° |
| argument of perigee: | 279.8984° |
| revolutions per day: | 15.27584508 |
| mean anomaly at epoch: | 80.1722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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