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 22782U 26159.53989962 +.00000000 +00000-0 -24839-5 0 00000
2 22782 82.5484 301.6184 0021309 230.7605 201.1513 13.84027318 05
| Epoch (UTC): | 08 June 2026 12:57:27 |
| Eccentricity: | 0.0021309 |
| inclination: | 82.5484° |
| perigee height: | 934 km |
| apogee height: | 965 km |
| right ascension of ascending node: | 301.6184° |
| argument of perigee: | 230.7605° |
| revolutions per day: | 13.84027318 |
| mean anomaly at epoch: | 201.1513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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