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 62925U 26145.45847461 +.00000000 +00000-0 +63229-3 0 00009
2 62925 43.0027 55.2705 0001441 273.3813 86.6874 15.27597041 03
| Epoch (UTC): | 25 May 2026 11:00:12 |
| Eccentricity: | 0.0001441 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 55.2705° |
| argument of perigee: | 273.3813° |
| revolutions per day: | 15.27597041 |
| mean anomaly at epoch: | 86.6874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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