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 57866U 26145.54023155 +.00000000 +00000-0 +48307-4 0 00004
2 57866 42.9979 210.9393 0001357 278.9873 81.0825 15.27579030 04
| Epoch (UTC): | 25 May 2026 12:57:56 |
| Eccentricity: | 0.0001357 |
| inclination: | 42.9979° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 210.9393° |
| argument of perigee: | 278.9873° |
| revolutions per day: | 15.27579030 |
| mean anomaly at epoch: | 81.0825° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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