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 32750U 08014A 26010.73675071 0.00008500 00000-0 31147-3 0 00
2 32750 98.1348 28.4344 0002081 287.3060 72.6939 15.28033546 07
| Epoch (UTC): | 10 January 2026 17:40:55 |
| Eccentricity: | 0.0002081 |
| inclination: | 98.1348° |
| perigee height: | 480 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 28.4344° |
| argument of perigee: | 287.3060° |
| revolutions per day: | 15.28033546 |
| mean anomaly at epoch: | 72.6939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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