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 26040.63701083 +.00000000 +00000-0 +12440-3 0 00009
2 29092 97.7580 64.5016 0001424 88.9748 271.1631 14.87522967 09
| Epoch (UTC): | 09 February 2026 15:17:17 |
| Eccentricity: | 0.0001424 |
| inclination: | 97.7580° |
| perigee height: | 605 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 64.5016° |
| argument of perigee: | 88.9748° |
| revolutions per day: | 14.87522967 |
| mean anomaly at epoch: | 271.1631° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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