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 66135U 26066.37096258 +.00000000 +00000-0 +12304-2 0 00006
2 66135 53.1598 50.5276 0001258 80.7186 279.3957 15.30229876 00
| Epoch (UTC): | 07 March 2026 08:54:11 |
| Eccentricity: | 0.0001258 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 50.5276° |
| argument of perigee: | 80.7186° |
| revolutions per day: | 15.30229876 |
| mean anomaly at epoch: | 279.3957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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