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 44801U 26145.58589512 +.00000000 +00000-0 +00000-0 0 00001
2 44801 0.0419 12.8824 0002000 58.4120 33.8302 1.00270131 04
| Epoch (UTC): | 25 May 2026 14:03:41 |
| Eccentricity: | 0.0002000 |
| inclination: | 0.0419° |
| perigee height: | 35779 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 12.8824° |
| argument of perigee: | 58.4120° |
| revolutions per day: | 1.00270131 |
| mean anomaly at epoch: | 33.8302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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