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 33844U 93036CM 24281.01298498 .00004593 00000-0 16991-2 0 9990
2 33844 74.0660 120.0614 0050558 251.0620 266.9842 14.31920287815840
| Epoch (UTC): | 07 October 2024 00:18:41 |
| Eccentricity: | 0.0050558 |
| inclination: | 74.0660° |
| perigee height: | 749 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 120.0614° |
| argument of perigee: | 251.0620° |
| revolutions per day: | 14.31920287 |
| mean anomaly at epoch: | 266.9842° |
| orbit number at epoch: | 81584 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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