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 44424U 26145.73274505 +.00000000 +00000-0 +27170-3 0 00002
2 44424 97.5881 224.9775 0043794 122.0814 238.4685 15.20425584 01
| Epoch (UTC): | 25 May 2026 17:35:09 |
| Eccentricity: | 0.0043794 |
| inclination: | 97.5881° |
| perigee height: | 474 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 224.9775° |
| argument of perigee: | 122.0814° |
| revolutions per day: | 15.20425584 |
| mean anomaly at epoch: | 238.4685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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