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 39249U 26145.57580159 +.00000000 +00000-0 +57566-3 0 00000
2 39249 82.4845 357.4814 0015613 263.0452 96.8852 12.42891405 04
| Epoch (UTC): | 25 May 2026 13:49:09 |
| Eccentricity: | 0.0015613 |
| inclination: | 82.4845° |
| perigee height: | 1482 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 357.4814° |
| argument of perigee: | 263.0452° |
| revolutions per day: | 12.42891405 |
| mean anomaly at epoch: | 96.8852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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