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 57612U 26145.34251791 +.00000000 +00000-0 +15154-4 0 00004
2 57612 43.0037 8.3216 0001085 266.1596 93.9131 15.27578655 06
| Epoch (UTC): | 25 May 2026 08:13:13 |
| Eccentricity: | 0.0001085 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 8.3216° |
| argument of perigee: | 266.1596° |
| revolutions per day: | 15.27578655 |
| mean anomaly at epoch: | 93.9131° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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