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 26022.47456816 +.00000000 +00000-0 +19322-3 0 00008
2 29092 97.7587 46.7468 0001468 85.6181 274.5203 14.87470761 08
| Epoch (UTC): | 22 January 2026 11:23:22 |
| Eccentricity: | 0.0001468 |
| inclination: | 97.7587° |
| perigee height: | 605 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 46.7468° |
| argument of perigee: | 85.6181° |
| revolutions per day: | 14.87470761 |
| mean anomaly at epoch: | 274.5203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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