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 57117U 26145.56888260 +.00000000 +00000-0 -74615-5 0 00004
2 57117 43.0018 207.0753 0001376 265.1153 94.9542 15.27573732 08
| Epoch (UTC): | 25 May 2026 13:39:11 |
| Eccentricity: | 0.0001376 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 207.0753° |
| argument of perigee: | 265.1153° |
| revolutions per day: | 15.27573732 |
| mean anomaly at epoch: | 94.9542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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