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 26037.60997808 +.00000000 +00000-0 +14872-3 0 00005
2 29092 97.7580 61.5425 0001426 88.2714 271.8665 14.87516493 09
| Epoch (UTC): | 06 February 2026 14:38:22 |
| Eccentricity: | 0.0001426 |
| inclination: | 97.7580° |
| perigee height: | 605 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 61.5425° |
| argument of perigee: | 88.2714° |
| revolutions per day: | 14.87516493 |
| mean anomaly at epoch: | 271.8665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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