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 26018.61028002 +.00000000 +00000-0 +43853-4 0 00005
2 20511 82.5209 269.9069 0014921 255.9952 103.9604 14.82088347 00
| Epoch (UTC): | 18 January 2026 14:38:48 |
| Eccentricity: | 0.0014921 |
| inclination: | 82.5209° |
| perigee height: | 612 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 269.9069° |
| argument of perigee: | 255.9952° |
| revolutions per day: | 14.82088347 |
| mean anomaly at epoch: | 103.9604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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