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 26039.82980353 +.00000000 +00000-0 +12638-3 0 00006
2 29092 97.7580 63.7125 0001418 89.0704 271.0675 14.87520967 03
| Epoch (UTC): | 08 February 2026 19:54:55 |
| Eccentricity: | 0.0001418 |
| inclination: | 97.7580° |
| perigee height: | 605 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 63.7125° |
| argument of perigee: | 89.0704° |
| revolutions per day: | 14.87520967 |
| mean anomaly at epoch: | 271.0675° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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