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 59079U 26145.52169941 +.00000000 +00000-0 +18682-4 0 00007
2 59079 43.0003 236.6556 0001621 266.7701 93.2966 15.27576069 07
| Epoch (UTC): | 25 May 2026 12:31:14 |
| Eccentricity: | 0.0001621 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.6556° |
| argument of perigee: | 266.7701° |
| revolutions per day: | 15.27576069 |
| mean anomaly at epoch: | 93.2966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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