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 44529U 26145.49345294 +.00000000 +00000-0 +93839-4 0 00001
2 44529 98.6029 274.1617 0014426 83.3136 276.9697 14.48367056 09
| Epoch (UTC): | 25 May 2026 11:50:34 |
| Eccentricity: | 0.0014426 |
| inclination: | 98.6029° |
| perigee height: | 721 km |
| apogee height: | 741 km |
| right ascension of ascending node: | 274.1617° |
| argument of perigee: | 83.3136° |
| revolutions per day: | 14.48367056 |
| mean anomaly at epoch: | 276.9697° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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