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 26041.04061404 +.00000000 +00000-0 +11943-3 0 00008
2 29092 97.7580 64.8961 0001423 89.0634 271.0746 14.87523771 06
| Epoch (UTC): | 10 February 2026 00:58:29 |
| Eccentricity: | 0.0001423 |
| inclination: | 97.7580° |
| perigee height: | 605 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 64.8961° |
| argument of perigee: | 89.0634° |
| revolutions per day: | 14.87523771 |
| mean anomaly at epoch: | 271.0746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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