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 26101.47954537 +.00000000 +00000-0 +29432-3 0 00005
2 32785 97.8247 81.5608 0007216 252.2826 107.7615 15.08834377 08
| Epoch (UTC): | 11 April 2026 11:30:32 |
| Eccentricity: | 0.0007216 |
| inclination: | 97.8247° |
| perigee height: | 535 km |
| apogee height: | 545 km |
| right ascension of ascending node: | 81.5608° |
| argument of perigee: | 252.2826° |
| revolutions per day: | 15.08834377 |
| mean anomaly at epoch: | 107.7615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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