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 20692U 26019.10679931 +.00000000 +00000-0 +49592-3 0 00008
2 20692 63.2936 252.5015 0879803 81.8184 288.1571 13.62771682 00
| Epoch (UTC): | 19 January 2026 02:33:47 |
| Eccentricity: | 0.0879803 |
| inclination: | 63.2936° |
| perigee height: | 374 km |
| apogee height: | 1677 km |
| right ascension of ascending node: | 252.5015° |
| argument of perigee: | 81.8184° |
| revolutions per day: | 13.62771682 |
| mean anomaly at epoch: | 288.1571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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