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 57890U 26145.65838227 +.00000000 +00000-0 +29072-3 0 00004
2 57890 34.9952 4.8779 0006140 223.4405 136.5824 15.17555362 08
| Epoch (UTC): | 25 May 2026 15:48:04 |
| Eccentricity: | 0.0006140 |
| inclination: | 34.9952° |
| perigee height: | 509 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 4.8779° |
| argument of perigee: | 223.4405° |
| revolutions per day: | 15.17555362 |
| mean anomaly at epoch: | 136.5824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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