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 20929U 26146.01552816 +.00000000 +00000-0 +00000-0 0 00002
2 20929 14.0173 344.2052 0004632 76.7658 281.5804 0.98396295 03
| Epoch (UTC): | 26 May 2026 00:22:21 |
| Eccentricity: | 0.0004632 |
| inclination: | 14.0173° |
| perigee height: | 36301 km |
| apogee height: | 36340 km |
| right ascension of ascending node: | 344.2052° |
| argument of perigee: | 76.7658° |
| revolutions per day: | 0.98396295 |
| mean anomaly at epoch: | 281.5804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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