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 26039.49346683 +.00000000 +00000-0 +13107-3 0 00003
2 29092 97.7580 63.3837 0001429 89.3574 270.7806 14.87520370 09
| Epoch (UTC): | 08 February 2026 11:50:35 |
| Eccentricity: | 0.0001429 |
| inclination: | 97.7580° |
| perigee height: | 605 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 63.3837° |
| argument of perigee: | 89.3574° |
| revolutions per day: | 14.87520370 |
| mean anomaly at epoch: | 270.7806° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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