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 66526U 26145.44885671 +.00000000 +00000-0 +46048-3 0 00004
2 66526 42.9997 204.3634 0000807 266.2003 93.8757 15.27590573 06
| Epoch (UTC): | 25 May 2026 10:46:21 |
| Eccentricity: | 0.0000807 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.3634° |
| argument of perigee: | 266.2003° |
| revolutions per day: | 15.27590573 |
| mean anomaly at epoch: | 93.8757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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