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 29092U 26064.98734142 +.00000000 +00000-0 +12932-3 0 00001
2 29092 97.7557 88.3049 0001466 93.5226 266.6158 14.87575049 04
| Epoch (UTC): | 05 March 2026 23:41:46 |
| Eccentricity: | 0.0001466 |
| inclination: | 97.7557° |
| perigee height: | 604 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 88.3049° |
| argument of perigee: | 93.5226° |
| revolutions per day: | 14.87575049 |
| mean anomaly at epoch: | 266.6158° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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