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 26072.56107091 +.00000000 +00000-0 +55549-3 0 00005
2 32785 97.8203 52.1020 0009180 5.6192 354.5137 15.08433027 08
| Epoch (UTC): | 13 March 2026 13:27:56 |
| Eccentricity: | 0.0009180 |
| inclination: | 97.8203° |
| perigee height: | 535 km |
| apogee height: | 547 km |
| right ascension of ascending node: | 52.1020° |
| argument of perigee: | 5.6192° |
| revolutions per day: | 15.08433027 |
| mean anomaly at epoch: | 354.5137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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