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 58912U 26145.60218661 +.00000000 +00000-0 +22775-3 0 00002
2 58912 49.9894 97.8383 0004243 266.3619 93.6833 14.83150587 08
| Epoch (UTC): | 25 May 2026 14:27:08 |
| Eccentricity: | 0.0004243 |
| inclination: | 49.9894° |
| perigee height: | 616 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 97.8383° |
| argument of perigee: | 266.3619° |
| revolutions per day: | 14.83150587 |
| mean anomaly at epoch: | 93.6833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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