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 26039.56073434 +.00000000 +00000-0 +12599-3 0 00006
2 29092 97.7580 63.4495 0001431 89.4411 270.6969 14.87520246 05
| Epoch (UTC): | 08 February 2026 13:27:27 |
| Eccentricity: | 0.0001431 |
| inclination: | 97.7580° |
| perigee height: | 605 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 63.4495° |
| argument of perigee: | 89.4411° |
| revolutions per day: | 14.87520246 |
| mean anomaly at epoch: | 270.6969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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