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 57865U 26145.48640841 +.00000000 +00000-0 +86035-4 0 00003
2 57865 43.0016 211.3965 0001478 279.1075 80.9609 15.27583414 07
| Epoch (UTC): | 25 May 2026 11:40:25 |
| Eccentricity: | 0.0001478 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.3965° |
| argument of perigee: | 279.1075° |
| revolutions per day: | 15.27583414 |
| mean anomaly at epoch: | 80.9609° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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