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 57461U 26145.40996884 +.00000000 +00000-0 +20010-4 0 00009
2 57461 43.0013 270.2363 0001330 267.1002 92.9698 15.27574909 06
| Epoch (UTC): | 25 May 2026 09:50:21 |
| Eccentricity: | 0.0001330 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.2363° |
| argument of perigee: | 267.1002° |
| revolutions per day: | 15.27574909 |
| mean anomaly at epoch: | 92.9698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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