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 57950U 26145.38275140 +.00000000 +00000-0 +11246-3 0 00004
2 57950 53.1606 28.0859 0000895 96.3856 263.7247 15.30210422 01
| Epoch (UTC): | 25 May 2026 09:11:09 |
| Eccentricity: | 0.0000895 |
| inclination: | 53.1606° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 28.0859° |
| argument of perigee: | 96.3856° |
| revolutions per day: | 15.30210422 |
| mean anomaly at epoch: | 263.7247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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