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 66412U 26145.35094544 +.00000000 +00000-0 +75088-4 0 00006
2 66412 50.0064 17.5390 0000940 53.9701 306.1258 13.29323795 08
| Epoch (UTC): | 25 May 2026 08:25:21 |
| Eccentricity: | 0.0000940 |
| inclination: | 50.0064° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 17.5390° |
| argument of perigee: | 53.9701° |
| revolutions per day: | 13.29323795 |
| mean anomaly at epoch: | 306.1258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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