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 58281U 26145.23815322 +.00000000 +00000-0 +10896-2 0 00007
2 58281 97.3815 237.9561 0005660 212.8251 147.2663 15.74915011 03
| Epoch (UTC): | 25 May 2026 05:42:56 |
| Eccentricity: | 0.0005660 |
| inclination: | 97.3815° |
| perigee height: | 341 km |
| apogee height: | 349 km |
| right ascension of ascending node: | 237.9561° |
| argument of perigee: | 212.8251° |
| revolutions per day: | 15.74915011 |
| mean anomaly at epoch: | 147.2663° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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