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 26159.12657244 +.00000000 +00000-0 +13722-4 0 00007
2 22782 82.5490 301.9463 0021248 231.8374 301.8320 13.84027382 07
| Epoch (UTC): | 08 June 2026 03:02:15 |
| Eccentricity: | 0.0021248 |
| inclination: | 82.5490° |
| perigee height: | 934 km |
| apogee height: | 965 km |
| right ascension of ascending node: | 301.9463° |
| argument of perigee: | 231.8374° |
| revolutions per day: | 13.84027382 |
| mean anomaly at epoch: | 301.8320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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