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 23089.89316168 .00011496 00000-0 10378-2 0 9999
2 32791 97.6491 62.8659 0010852 323.5881 36.4601 14.95619044810037
| Epoch (UTC): | 30 March 2023 21:26:09 |
| Eccentricity: | 0.0010852 |
| inclination: | 97.6491° |
| perigee height: | 573 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 62.8659° |
| argument of perigee: | 323.5881° |
| revolutions per day: | 14.95619044 |
| mean anomaly at epoch: | 36.4601° |
| orbit number at epoch: | 81003 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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