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 57083U 26145.34718574 +.00000000 +00000-0 +28370-4 0 00007
2 57083 43.0029 23.2377 0001234 271.4970 88.5741 15.27578406 05
| Epoch (UTC): | 25 May 2026 08:19:56 |
| Eccentricity: | 0.0001234 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 23.2377° |
| argument of perigee: | 271.4970° |
| revolutions per day: | 15.27578406 |
| mean anomaly at epoch: | 88.5741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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