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 32788U 08021F 22272.92012465 .00005413 00000-0 45955-3 0 9997
2 32788 97.5455 254.6362 0012617 123.2836 236.9597 14.98240850784073
| Epoch (UTC): | 29 September 2022 22:04:58 |
| Eccentricity: | 0.0012617 |
| inclination: | 97.5455° |
| perigee height: | 563 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 254.6362° |
| argument of perigee: | 123.2836° |
| revolutions per day: | 14.98240850 |
| mean anomaly at epoch: | 236.9597° |
| orbit number at epoch: | 78407 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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