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 35580U 93036ALX 23338.72630521 .00002189 00000-0 15965-2 0 9995
2 35580 73.9090 349.8002 0290781 137.0508 225.3721 13.78394106520537
| Epoch (UTC): | 04 December 2023 17:25:52 |
| Eccentricity: | 0.0290781 |
| inclination: | 73.9090° |
| perigee height: | 756 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 349.8002° |
| argument of perigee: | 137.0508° |
| revolutions per day: | 13.78394106 |
| mean anomaly at epoch: | 225.3721° |
| orbit number at epoch: | 52053 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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