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 66118U 26145.41028687 +.00000000 +00000-0 +81386-3 0 00008
2 66118 53.1587 43.4913 0001146 82.9155 277.1976 15.30215032 00
| Epoch (UTC): | 25 May 2026 09:50:48 |
| Eccentricity: | 0.0001146 |
| inclination: | 53.1587° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.4913° |
| argument of perigee: | 82.9155° |
| revolutions per day: | 15.30215032 |
| mean anomaly at epoch: | 277.1976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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