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 32785U 26102.14272219 +.00000000 +00000-0 +28506-3 0 00001
2 32785 97.8246 82.2367 0007204 249.4103 110.6352 15.08840801 00
| Epoch (UTC): | 12 April 2026 03:25:31 |
| Eccentricity: | 0.0007204 |
| inclination: | 97.8246° |
| perigee height: | 535 km |
| apogee height: | 545 km |
| right ascension of ascending node: | 82.2367° |
| argument of perigee: | 249.4103° |
| revolutions per day: | 15.08840801 |
| mean anomaly at epoch: | 110.6352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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