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 58889U 26145.47960051 +.00000000 +00000-0 +79866-4 0 00001
2 58889 53.1625 325.3388 0001141 93.2433 266.8700 15.34385707 07
| Epoch (UTC): | 25 May 2026 11:30:37 |
| Eccentricity: | 0.0001141 |
| inclination: | 53.1625° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 325.3388° |
| argument of perigee: | 93.2433° |
| revolutions per day: | 15.34385707 |
| mean anomaly at epoch: | 266.8700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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