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 12172U 78026M 24357.02671964 .00000791 00000-0 34865-3 0 9998
2 12172 98.8283 14.8185 0059503 25.4056 3.0875 14.25284018274724
| Epoch (UTC): | 22 December 2024 00:38:28 |
| Eccentricity: | 0.0059503 |
| inclination: | 98.8283° |
| perigee height: | 765 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 14.8185° |
| argument of perigee: | 25.4056° |
| revolutions per day: | 14.25284018 |
| mean anomaly at epoch: | 3.0875° |
| orbit number at epoch: | 27472 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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