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 55543U 22151YR 24357.54293791 .00010627 00000-0 24190-2 0 9998
2 55543 98.5646 15.0143 0148113 167.2524 193.2480 14.49494534105540
| Epoch (UTC): | 22 December 2024 13:01:49 |
| Eccentricity: | 0.0148113 |
| inclination: | 98.5646° |
| perigee height: | 622 km |
| apogee height: | 832 km |
| right ascension of ascending node: | 15.0143° |
| argument of perigee: | 167.2524° |
| revolutions per day: | 14.49494534 |
| mean anomaly at epoch: | 193.2480° |
| orbit number at epoch: | 10554 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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