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 66182U 26144.99685565 +.00000000 +00000-0 +77425-3 0 00004
2 66182 53.1583 251.0328 0000925 258.3862 101.7035 15.30212311 07
| Epoch (UTC): | 24 May 2026 23:55:28 |
| Eccentricity: | 0.0000925 |
| inclination: | 53.1583° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 251.0328° |
| argument of perigee: | 258.3862° |
| revolutions per day: | 15.30212311 |
| mean anomaly at epoch: | 101.7035° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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