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 19046U 88032B 24287.93540868 .00008460 00000-0 48902-3 0 9991
2 19046 97.4625 266.6913 0029444 205.9029 154.0729 15.12161954974540
| Epoch (UTC): | 13 October 2024 22:26:59 |
| Eccentricity: | 0.0029444 |
| inclination: | 97.4625° |
| perigee height: | 509 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 266.6913° |
| argument of perigee: | 205.9029° |
| revolutions per day: | 15.12161954 |
| mean anomaly at epoch: | 154.0729° |
| orbit number at epoch: | 97454 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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