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 58943U 26144.93695882 +.00000000 +00000-0 +75417-4 0 00007
2 58943 53.1606 313.2345 0001203 81.8579 278.2558 15.30199613 02
| Epoch (UTC): | 24 May 2026 22:29:13 |
| Eccentricity: | 0.0001203 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.2345° |
| argument of perigee: | 81.8579° |
| revolutions per day: | 15.30199613 |
| mean anomaly at epoch: | 278.2558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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