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 18753U 87020AE 24357.85175993 .00000264 00000-0 19612-2 0 9992
2 18753 73.4452 136.5669 0023946 80.7161 36.8823 12.45685062681783
| Epoch (UTC): | 22 December 2024 20:26:32 |
| Eccentricity: | 0.0023946 |
| inclination: | 73.4452° |
| perigee height: | 1464 km |
| apogee height: | 1501 km |
| right ascension of ascending node: | 136.5669° |
| argument of perigee: | 80.7161° |
| revolutions per day: | 12.45685062 |
| mean anomaly at epoch: | 36.8823° |
| orbit number at epoch: | 68178 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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