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 24151U 94029HA 24277.84297927 .00011172 00000-0 19235-2 0 9991
2 24151 82.0174 70.3641 0155688 203.7695 155.6265 14.60765982502086
| Epoch (UTC): | 03 October 2024 20:13:53 |
| Eccentricity: | 0.0155688 |
| inclination: | 82.0174° |
| perigee height: | 580 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 70.3641° |
| argument of perigee: | 203.7695° |
| revolutions per day: | 14.60765982 |
| mean anomaly at epoch: | 155.6265° |
| orbit number at epoch: | 50208 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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