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 57062U 26145.34589641 +.00000000 +00000-0 +24699-4 0 00005
2 57062 43.0043 23.2116 0001193 257.6791 102.3928 15.27576887 03
| Epoch (UTC): | 25 May 2026 08:18:05 |
| Eccentricity: | 0.0001193 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 23.2116° |
| argument of perigee: | 257.6791° |
| revolutions per day: | 15.27576887 |
| mean anomaly at epoch: | 102.3928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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