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 66180U 26145.58047326 +.00000000 +00000-0 +20454-3 0 00005
2 66180 53.1565 248.2777 0000873 295.2514 64.8397 15.30192781 05
| Epoch (UTC): | 25 May 2026 13:55:52 |
| Eccentricity: | 0.0000873 |
| inclination: | 53.1565° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.2777° |
| argument of perigee: | 295.2514° |
| revolutions per day: | 15.30192781 |
| mean anomaly at epoch: | 64.8397° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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