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 22141.90801911 .00009158 00000-0 79380-3 0 9991
2 32788 97.5321 128.1691 0010337 200.8235 159.2568 14.97267530764567
| Epoch (UTC): | 21 May 2022 21:47:32 |
| Eccentricity: | 0.0010337 |
| inclination: | 97.5321° |
| perigee height: | 568 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 128.1691° |
| argument of perigee: | 200.8235° |
| revolutions per day: | 14.97267530 |
| mean anomaly at epoch: | 159.2568° |
| orbit number at epoch: | 76456 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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