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 26017.19169118 +.00000000 +00000-0 +59514-4 0 00004
2 22782 82.5470 54.6346 0021008 272.4172 151.9123 13.84016493 04
| Epoch (UTC): | 17 January 2026 04:36:02 |
| Eccentricity: | 0.0021008 |
| inclination: | 82.5470° |
| perigee height: | 934 km |
| apogee height: | 965 km |
| right ascension of ascending node: | 54.6346° |
| argument of perigee: | 272.4172° |
| revolutions per day: | 13.84016493 |
| mean anomaly at epoch: | 151.9123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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