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 22178.70782959 .00001076 00000-0 11813-3 0 9994
2 32785 97.6576 149.2315 0012088 192.6341 167.4576 14.89623078768080
| Epoch (UTC): | 27 June 2022 16:59:16 |
| Eccentricity: | 0.0012088 |
| inclination: | 97.6576° |
| perigee height: | 590 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 149.2315° |
| argument of perigee: | 192.6341° |
| revolutions per day: | 14.89623078 |
| mean anomaly at epoch: | 167.4576° |
| orbit number at epoch: | 76808 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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