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 41850U 26145.35720874 +.00000000 +00000-0 +24079-3 0 00000
2 41850 98.0706 10.3681 0001133 55.0631 305.0708 15.19419219 02
| Epoch (UTC): | 25 May 2026 08:34:22 |
| Eccentricity: | 0.0001133 |
| inclination: | 98.0706° |
| perigee height: | 507 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 10.3681° |
| argument of perigee: | 55.0631° |
| revolutions per day: | 15.19419219 |
| mean anomaly at epoch: | 305.0708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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