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 51284U 22007A 24358.20632046 .00001744 00000-0 19405-3 0 9994
2 51284 97.8094 2.3787 0001639 88.9648 271.1757 14.88408985158007
| Epoch (UTC): | 23 December 2024 04:57:06 |
| Eccentricity: | 0.0001639 |
| inclination: | 97.8094° |
| perigee height: | 602 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 2.3787° |
| argument of perigee: | 88.9648° |
| revolutions per day: | 14.88408985 |
| mean anomaly at epoch: | 271.1757° |
| orbit number at epoch: | 15800 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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