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 08520U 75124B 24283.83584967 .00000546 00000-0 30608-3 0 9998
2 08520 81.2828 104.9503 0026506 352.3856 7.6908 14.09260002507128
| Epoch (UTC): | 09 October 2024 20:03:37 |
| Eccentricity: | 0.0026506 |
| inclination: | 81.2828° |
| perigee height: | 843 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 104.9503° |
| argument of perigee: | 352.3856° |
| revolutions per day: | 14.09260002 |
| mean anomaly at epoch: | 7.6908° |
| orbit number at epoch: | 50712 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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