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 26040.03160543 +.00000000 +00000-0 +11946-3 0 00003
2 29092 97.7579 63.9098 0001422 89.2600 270.8779 14.87521186 00
| Epoch (UTC): | 09 February 2026 00:45:30 |
| Eccentricity: | 0.0001422 |
| inclination: | 97.7579° |
| perigee height: | 605 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 63.9098° |
| argument of perigee: | 89.2600° |
| revolutions per day: | 14.87521186 |
| mean anomaly at epoch: | 270.8779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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