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 data is extracted from the following two-line orbital elements,
1 32785U 08021C 22221.83097691 .00001421 00000-0 15366-3 0 9990
2 32785 97.6612 191.0040 0014088 60.7525 299.5100 14.89739053774439
| Epoch (UTC): | 09 August 2022 19:56:36 |
| Eccentricity: | 0.0014088 |
| inclination: | 97.6612° |
| perigee height: | 589 km |
| apogee height: | 608 km |
| right ascension of ascending node: | 191.0040° |
| argument of perigee: | 60.7525° |
| revolutions per day: | 14.89739053 |
| mean anomaly at epoch: | 299.5100° |
| orbit number at epoch: | 77443 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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