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 39251U 26145.61966823 +.00000000 +00000-0 +39539-4 0 00005
2 39251 82.4913 0.3643 0016423 264.2737 95.6470 12.42913968 08
| Epoch (UTC): | 25 May 2026 14:52:19 |
| Eccentricity: | 0.0016423 |
| inclination: | 82.4913° |
| perigee height: | 1481 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 0.3643° |
| argument of perigee: | 264.2737° |
| revolutions per day: | 12.42913968 |
| mean anomaly at epoch: | 95.6470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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