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 58942U 26145.45767516 +.00000000 +00000-0 +32726-4 0 00004
2 58942 53.1604 312.9153 0001366 92.8364 267.2794 15.31702198 05
| Epoch (UTC): | 25 May 2026 10:59:03 |
| Eccentricity: | 0.0001366 |
| inclination: | 53.1604° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 312.9153° |
| argument of perigee: | 92.8364° |
| revolutions per day: | 15.31702198 |
| mean anomaly at epoch: | 267.2794° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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