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 32706U 08010A 25093.58670192 0.00000000 00000-0 00000-0 0 07
2 32706 63.6449 14.3526 7200177 268.6605 15.7709 2.00636144 05
| Epoch (UTC): | 03 April 2025 14:04:51 |
| Eccentricity: | 0.7200177 |
| inclination: | 63.6449° |
| perigee height: | 1056 km |
| apogee height: | 39295 km |
| right ascension of ascending node: | 14.3526° |
| argument of perigee: | 268.6605° |
| revolutions per day: | 2.00636144 |
| mean anomaly at epoch: | 15.7709° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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