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 20510U 26074.66330747 +.00000000 +00000-0 +20824-3 0 00005
2 20510 82.5010 325.9598 0004525 278.8577 104.6989 15.15704783 05
| Epoch (UTC): | 15 March 2026 15:55:09 |
| Eccentricity: | 0.0004525 |
| inclination: | 82.5010° |
| perigee height: | 516 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 325.9598° |
| argument of perigee: | 278.8577° |
| revolutions per day: | 15.15704783 |
| mean anomaly at epoch: | 104.6989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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