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 26150.87964264 +.00000000 +00000-0 +43648-3 0 00006
2 32785 97.8267 131.9415 0010808 88.8154 271.4312 15.09269731 04
| Epoch (UTC): | 30 May 2026 21:06:41 |
| Eccentricity: | 0.0010808 |
| inclination: | 97.8267° |
| perigee height: | 531 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 131.9415° |
| argument of perigee: | 88.8154° |
| revolutions per day: | 15.09269731 |
| mean anomaly at epoch: | 271.4312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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