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 26020.32193656 +.00000000 +00000-0 +14564-3 0 00003
2 29092 97.7588 44.6425 0001481 85.8708 274.2677 14.87461468 07
| Epoch (UTC): | 20 January 2026 07:43:35 |
| Eccentricity: | 0.0001481 |
| inclination: | 97.7588° |
| perigee height: | 605 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 44.6425° |
| argument of perigee: | 85.8708° |
| revolutions per day: | 14.87461468 |
| mean anomaly at epoch: | 274.2677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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