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 26070.77457639 +.00000000 +00000-0 +26073-3 0 00005
2 20510 82.5014 329.7996 0004871 296.2945 121.9763 15.15668566 00
| Epoch (UTC): | 11 March 2026 18:35:23 |
| Eccentricity: | 0.0004871 |
| inclination: | 82.5014° |
| perigee height: | 516 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 329.7996° |
| argument of perigee: | 296.2945° |
| revolutions per day: | 15.15668566 |
| mean anomaly at epoch: | 121.9763° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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