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 66080U 26145.57622939 +.00000000 +00000-0 +56104-3 0 00003
2 66080 53.1578 248.0971 0001616 327.1068 32.9832 15.30184964 01
| Epoch (UTC): | 25 May 2026 13:49:46 |
| Eccentricity: | 0.0001616 |
| inclination: | 53.1578° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.0971° |
| argument of perigee: | 327.1068° |
| revolutions per day: | 15.30184964 |
| mean anomaly at epoch: | 32.9832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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