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 57992U 26145.61102220 +.00000000 +00000-0 +39519-3 0 00007
2 57992 42.9991 352.3707 0001228 268.6141 91.4570 15.27582189 00
| Epoch (UTC): | 25 May 2026 14:39:52 |
| Eccentricity: | 0.0001228 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 352.3707° |
| argument of perigee: | 268.6141° |
| revolutions per day: | 15.27582189 |
| mean anomaly at epoch: | 91.4570° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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