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 57942U 26145.40808150 +.00000000 +00000-0 +57812-4 0 00001
2 57942 53.1612 28.1317 0001347 85.9376 274.1779 15.30188909 03
| Epoch (UTC): | 25 May 2026 09:47:38 |
| Eccentricity: | 0.0001347 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 28.1317° |
| argument of perigee: | 85.9376° |
| revolutions per day: | 15.30188909 |
| mean anomaly at epoch: | 274.1779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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