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 26017.63699590 +.00000000 +00000-0 +59909-4 0 00003
2 22782 82.5470 54.2809 0021006 271.0754 210.7172 13.84016545 09
| Epoch (UTC): | 17 January 2026 15:17:16 |
| Eccentricity: | 0.0021006 |
| inclination: | 82.5470° |
| perigee height: | 934 km |
| apogee height: | 965 km |
| right ascension of ascending node: | 54.2809° |
| argument of perigee: | 271.0754° |
| revolutions per day: | 13.84016545 |
| mean anomaly at epoch: | 210.7172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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