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 58372U 26145.39242458 +.00000000 +00000-0 +42206-4 0 00001
2 58372 43.0005 277.8039 0001315 279.4334 80.6369 15.27579092 06
| Epoch (UTC): | 25 May 2026 09:25:05 |
| Eccentricity: | 0.0001315 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.8039° |
| argument of perigee: | 279.4334° |
| revolutions per day: | 15.27579092 |
| mean anomaly at epoch: | 80.6369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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