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 58872U 26145.57683426 +.00000000 +00000-0 +58189-4 0 00007
2 58872 42.9989 174.5033 0001371 272.6833 87.3862 15.27583869 07
| Epoch (UTC): | 25 May 2026 13:50:38 |
| Eccentricity: | 0.0001371 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 174.5033° |
| argument of perigee: | 272.6833° |
| revolutions per day: | 15.27583869 |
| mean anomaly at epoch: | 87.3862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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