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 66501U 26145.42186875 +.00000000 +00000-0 +42573-3 0 00004
2 66501 43.0018 277.3962 0001736 268.6108 91.4545 15.27583523 09
| Epoch (UTC): | 25 May 2026 10:07:29 |
| Eccentricity: | 0.0001736 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.3962° |
| argument of perigee: | 268.6108° |
| revolutions per day: | 15.27583523 |
| mean anomaly at epoch: | 91.4545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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