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 26066.52436198 +.00000000 +00000-0 +61192-3 0 00008
2 32785 97.8210 45.9571 0009948 26.9118 333.2624 15.08336798 05
| Epoch (UTC): | 07 March 2026 12:35:04 |
| Eccentricity: | 0.0009948 |
| inclination: | 97.8210° |
| perigee height: | 534 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 45.9571° |
| argument of perigee: | 26.9118° |
| revolutions per day: | 15.08336798 |
| mean anomaly at epoch: | 333.2624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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