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 66120U 26145.00046068 +.00000000 +00000-0 +33907-3 0 00005
2 66120 53.1594 45.1969 0001183 62.8971 297.2150 15.30190689 02
| Epoch (UTC): | 25 May 2026 00:00:39 |
| Eccentricity: | 0.0001183 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 45.1969° |
| argument of perigee: | 62.8971° |
| revolutions per day: | 15.30190689 |
| mean anomaly at epoch: | 297.2150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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