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 26162.94544593 +.00000000 +00000-0 +30225-3 0 00003
2 32785 97.8271 144.2548 0010282 54.9018 305.3173 15.09404820 04
| Epoch (UTC): | 11 June 2026 22:41:26 |
| Eccentricity: | 0.0010282 |
| inclination: | 97.8271° |
| perigee height: | 531 km |
| apogee height: | 545 km |
| right ascension of ascending node: | 144.2548° |
| argument of perigee: | 54.9018° |
| revolutions per day: | 15.09404820 |
| mean anomaly at epoch: | 305.3173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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