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 57698U 26145.42399850 +.00000000 +00000-0 +81004-4 0 00003
2 57698 43.0071 44.9223 0001387 267.0809 92.9884 15.27577844 07
| Epoch (UTC): | 25 May 2026 10:10:33 |
| Eccentricity: | 0.0001387 |
| inclination: | 43.0071° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 44.9223° |
| argument of perigee: | 267.0809° |
| revolutions per day: | 15.27577844 |
| mean anomaly at epoch: | 92.9884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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