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 26132.57998904 +.00000000 +00000-0 +18328-3 0 00008
2 32785 97.8259 113.2726 0010022 141.3017 218.8931 15.09104326 04
| Epoch (UTC): | 12 May 2026 13:55:11 |
| Eccentricity: | 0.0010022 |
| inclination: | 97.8259° |
| perigee height: | 532 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 113.2726° |
| argument of perigee: | 141.3017° |
| revolutions per day: | 15.09104326 |
| mean anomaly at epoch: | 218.8931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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