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 53503C 22099AQ 24358.49840278 .00018025 00000+0 14068-2 0 3587
2 53503 97.6547 116.6078 0003679 238.3602 91.3944 15.01218475 19
| Epoch (UTC): | 23 December 2024 11:57:42 |
| Eccentricity: | 0.0003679 |
| inclination: | 97.6547° |
| perigee height: | 560 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 116.6078° |
| argument of perigee: | 238.3602° |
| revolutions per day: | 15.01218475 |
| mean anomaly at epoch: | 91.3944° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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