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 43485U 26145.63541850 +.00000000 +00000-0 +24682-3 0 00002
2 43485 97.8097 224.1866 0008775 186.3954 173.7152 14.87184284 01
| Epoch (UTC): | 25 May 2026 15:15:00 |
| Eccentricity: | 0.0008775 |
| inclination: | 97.8097° |
| perigee height: | 601 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 224.1866° |
| argument of perigee: | 186.3954° |
| revolutions per day: | 14.87184284 |
| mean anomaly at epoch: | 173.7152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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