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 20511U 26017.93513956 +.00000000 +00000-0 +44324-4 0 00000
2 20511 82.5210 270.5379 0014908 258.4454 101.5087 14.82087962 05
| Epoch (UTC): | 17 January 2026 22:26:36 |
| Eccentricity: | 0.0014908 |
| inclination: | 82.5210° |
| perigee height: | 612 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 270.5379° |
| argument of perigee: | 258.4454° |
| revolutions per day: | 14.82087962 |
| mean anomaly at epoch: | 101.5087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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