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 29349U 26145.53489846 +.00000000 +00000-0 +00000-0 0 00005
2 29349 1.7292 83.2506 0001847 11.4016 94.0852 1.00271230 01
| Epoch (UTC): | 25 May 2026 12:50:15 |
| Eccentricity: | 0.0001847 |
| inclination: | 1.7292° |
| perigee height: | 35779 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 83.2506° |
| argument of perigee: | 11.4016° |
| revolutions per day: | 1.00271230 |
| mean anomaly at epoch: | 94.0852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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