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 41925U 26145.38900823 +.00000000 +00000-0 +62949-5 0 00000
2 41925 86.3946 97.8381 0002367 87.9718 272.1749 14.34217757 06
| Epoch (UTC): | 25 May 2026 09:20:10 |
| Eccentricity: | 0.0002367 |
| inclination: | 86.3946° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 97.8381° |
| argument of perigee: | 87.9718° |
| revolutions per day: | 14.34217757 |
| mean anomaly at epoch: | 272.1749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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