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 29499U 06044A 19287.94882383 +.00000006 +00000-0 +22264-4 0 9995
2 29499 098.5615 337.7016 0000639 115.5050 012.5615 14.21485349673682
| Epoch (UTC): | 14 October 2019 22:46:18 |
| Eccentricity: | 0.0000639 |
| inclination: | 98.5615° |
| perigee height: | 820 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 337.7016° |
| argument of perigee: | 115.5050° |
| revolutions per day: | 14.21485349 |
| mean anomaly at epoch: | 12.5615° |
| orbit number at epoch: | 67368 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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