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 26071.63237005 +.00000000 +00000-0 +50286-3 0 00004
2 32785 97.8202 51.1568 0009260 8.7950 351.3438 15.08417853 06
| Epoch (UTC): | 12 March 2026 15:10:36 |
| Eccentricity: | 0.0009260 |
| inclination: | 97.8202° |
| perigee height: | 535 km |
| apogee height: | 547 km |
| right ascension of ascending node: | 51.1568° |
| argument of perigee: | 8.7950° |
| revolutions per day: | 15.08417853 |
| mean anomaly at epoch: | 351.3438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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