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 24339.85602793 .00020395 00000-0 12240-2 0 9994
2 32791 97.7113 311.0379 0007665 85.7879 274.4226 15.10935015902305
| Epoch (UTC): | 04 December 2024 20:32:40 |
| Eccentricity: | 0.0007665 |
| inclination: | 97.7113° |
| perigee height: | 528 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 311.0379° |
| argument of perigee: | 85.7879° |
| revolutions per day: | 15.10935015 |
| mean anomaly at epoch: | 274.4226° |
| orbit number at epoch: | 90230 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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