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 26039.18852845 +.00000000 +00000-0 +47020-3 0 00005
2 32785 97.8167 18.1535 0011331 104.2656 255.9831 15.07933794 02
| Epoch (UTC): | 08 February 2026 04:31:28 |
| Eccentricity: | 0.0011331 |
| inclination: | 97.8167° |
| perigee height: | 535 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 18.1535° |
| argument of perigee: | 104.2656° |
| revolutions per day: | 15.07933794 |
| mean anomaly at epoch: | 255.9831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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