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 22142.16388483 .00005077 00000-0 49888-3 0 9994
2 32791 97.6102 119.3739 0010813 279.4516 80.5481 14.92536164763350
| Epoch (UTC): | 22 May 2022 03:55:59 |
| Eccentricity: | 0.0010813 |
| inclination: | 97.6102° |
| perigee height: | 582 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 119.3739° |
| argument of perigee: | 279.4516° |
| revolutions per day: | 14.92536164 |
| mean anomaly at epoch: | 80.5481° |
| orbit number at epoch: | 76335 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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