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 32791U 08021J 22026.41846715 .00001485 00000-0 15239-3 0 9992
2 32791 97.5959 7.6489 0011805 308.4541 51.5618 14.91828604746019
| Epoch (UTC): | 26 January 2022 10:02:35 |
| Eccentricity: | 0.0011805 |
| inclination: | 97.5959° |
| perigee height: | 584 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 7.6489° |
| argument of perigee: | 308.4541° |
| revolutions per day: | 14.91828604 |
| mean anomaly at epoch: | 51.5618° |
| orbit number at epoch: | 74601 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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