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 56280U 22151ACY 24280.91423852 .00004195 00000-0 27674-2 0 9999
2 56280 98.8179 268.1725 0100550 328.6168 30.9021 13.99782979 79242
| Epoch (UTC): | 06 October 2024 21:56:30 |
| Eccentricity: | 0.0100550 |
| inclination: | 98.8179° |
| perigee height: | 821 km |
| apogee height: | 967 km |
| right ascension of ascending node: | 268.1725° |
| argument of perigee: | 328.6168° |
| revolutions per day: | 13.99782979 |
| mean anomaly at epoch: | 30.9021° |
| orbit number at epoch: | 7924 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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