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 26069.90761721 +.00000000 +00000-0 +47821-3 0 00009
2 32785 97.8204 49.4012 0009462 15.0610 345.0897 15.08392233 03
| Epoch (UTC): | 10 March 2026 21:46:58 |
| Eccentricity: | 0.0009462 |
| inclination: | 97.8204° |
| perigee height: | 535 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 49.4012° |
| argument of perigee: | 15.0610° |
| revolutions per day: | 15.08392233 |
| mean anomaly at epoch: | 345.0897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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