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 53504C 22099AR 24358.51368056 .00018710 00000+0 14598-2 0 3589
2 53504 97.6547 116.6361 0002419 228.5814 195.0138 15.01231787 10
| Epoch (UTC): | 23 December 2024 12:19:42 |
| Eccentricity: | 0.0002419 |
| inclination: | 97.6547° |
| perigee height: | 561 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 116.6361° |
| argument of perigee: | 228.5814° |
| revolutions per day: | 15.01231787 |
| mean anomaly at epoch: | 195.0138° |
| 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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