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 57895U 26145.28787979 +.00000000 +00000-0 +69669-3 0 00001
2 57895 42.9979 241.3885 0001654 260.6621 99.4043 15.27606979 07
| Epoch (UTC): | 25 May 2026 06:54:32 |
| Eccentricity: | 0.0001654 |
| inclination: | 42.9979° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 241.3885° |
| argument of perigee: | 260.6621° |
| revolutions per day: | 15.27606979 |
| mean anomaly at epoch: | 99.4043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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