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 29272U 26145.39523065 +.00000000 +00000-0 +00000-0 0 00006
2 29272 0.0216 40.8523 0001979 358.8593 113.5428 1.00272705 00
| Epoch (UTC): | 25 May 2026 09:29:07 |
| Eccentricity: | 0.0001979 |
| inclination: | 0.0216° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 40.8523° |
| argument of perigee: | 358.8593° |
| revolutions per day: | 1.00272705 |
| mean anomaly at epoch: | 113.5428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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