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 26044.94210000 +.00000000 +00000-0 +11332-3 0 00000
2 29092 97.7576 68.7099 0001421 89.9451 270.1928 14.87532255 09
| Epoch (UTC): | 13 February 2026 22:36:37 |
| Eccentricity: | 0.0001421 |
| inclination: | 97.7576° |
| perigee height: | 605 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 68.7099° |
| argument of perigee: | 89.9451° |
| revolutions per day: | 14.87532255 |
| mean anomaly at epoch: | 270.1928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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