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 32787U 08021E 24256.99736925 .00064531 00000-0 32335-2 0 9994
2 32787 97.6290 233.5635 0004987 239.7246 120.3494 15.17094408891077
| Epoch (UTC): | 12 September 2024 23:56:12 |
| Eccentricity: | 0.0004987 |
| inclination: | 97.6290° |
| perigee height: | 511 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 233.5635° |
| argument of perigee: | 239.7246° |
| revolutions per day: | 15.17094408 |
| mean anomaly at epoch: | 120.3494° |
| orbit number at epoch: | 89107 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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