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 36660U 99025DYE 24258.80668679 .00004057 00000-0 21890-2 0 9995
2 36660 98.6325 269.6977 0050955 88.8453 271.8557 14.12543091830086
| Epoch (UTC): | 14 September 2024 19:21:37 |
| Eccentricity: | 0.0050955 |
| inclination: | 98.6325° |
| perigee height: | 814 km |
| apogee height: | 887 km |
| right ascension of ascending node: | 269.6977° |
| argument of perigee: | 88.8453° |
| revolutions per day: | 14.12543091 |
| mean anomaly at epoch: | 271.8557° |
| orbit number at epoch: | 83008 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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