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 22784U 26159.50953287 +.00000000 +00000-0 +28313-4 0 00009
2 22784 82.5500 306.7594 0020794 245.6397 182.2212 13.83549565 04
| Epoch (UTC): | 08 June 2026 12:13:43 |
| Eccentricity: | 0.0020794 |
| inclination: | 82.5500° |
| perigee height: | 936 km |
| apogee height: | 967 km |
| right ascension of ascending node: | 306.7594° |
| argument of perigee: | 245.6397° |
| revolutions per day: | 13.83549565 |
| mean anomaly at epoch: | 182.2212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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