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 20578U 26066.78993742 +.00000000 +00000-0 +86017-4 0 00000
2 20578 82.9469 154.6489 0014138 71.9713 48.8666 13.76636490 07
| Epoch (UTC): | 07 March 2026 18:57:30 |
| Eccentricity: | 0.0014138 |
| inclination: | 82.9469° |
| perigee height: | 965 km |
| apogee height: | 986 km |
| right ascension of ascending node: | 154.6489° |
| argument of perigee: | 71.9713° |
| revolutions per day: | 13.76636490 |
| mean anomaly at epoch: | 48.8666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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