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 57620U 26145.03486867 +.00000000 +00000-0 +39616-3 0 00001
2 57620 43.0013 10.3162 0001105 266.8879 93.1847 15.27566658 02
| Epoch (UTC): | 25 May 2026 00:50:12 |
| Eccentricity: | 0.0001105 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 10.3162° |
| argument of perigee: | 266.8879° |
| revolutions per day: | 15.27566658 |
| mean anomaly at epoch: | 93.1847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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