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 57825U 26145.53502197 +.00000000 +00000-0 +20921-4 0 00008
2 57825 43.0010 159.9569 0001468 271.5910 88.4773 15.27575235 04
| Epoch (UTC): | 25 May 2026 12:50:25 |
| Eccentricity: | 0.0001468 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 159.9569° |
| argument of perigee: | 271.5910° |
| revolutions per day: | 15.27575235 |
| mean anomaly at epoch: | 88.4773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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