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 37641U 78026JC 24277.85210305 .00008681 00000-0 32604-2 0 9990
2 37641 98.8180 290.9859 0074521 86.4062 274.5639 14.30274785266498
| Epoch (UTC): | 03 October 2024 20:27:01 |
| Eccentricity: | 0.0074521 |
| inclination: | 98.8180° |
| perigee height: | 737 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 290.9859° |
| argument of perigee: | 86.4062° |
| revolutions per day: | 14.30274785 |
| mean anomaly at epoch: | 274.5639° |
| orbit number at epoch: | 26649 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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