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 26075.21444959 +.00000000 +00000-0 +43509-3 0 00000
2 32785 97.8210 54.8033 0008883 357.3882 2.7298 15.08473480 08
| Epoch (UTC): | 16 March 2026 05:08:48 |
| Eccentricity: | 0.0008883 |
| inclination: | 97.8210° |
| perigee height: | 535 km |
| apogee height: | 547 km |
| right ascension of ascending node: | 54.8033° |
| argument of perigee: | 357.3882° |
| revolutions per day: | 15.08473480 |
| mean anomaly at epoch: | 2.7298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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