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 17526U 87017B 24287.72155468 .00000216 00000-0 20169-3 0 9995
2 17526 82.9046 200.3169 0041400 37.7985 322.6067 13.77107222874154
| Epoch (UTC): | 13 October 2024 17:19:02 |
| Eccentricity: | 0.0041400 |
| inclination: | 82.9046° |
| perigee height: | 944 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 200.3169° |
| argument of perigee: | 37.7985° |
| revolutions per day: | 13.77107222 |
| mean anomaly at epoch: | 322.6067° |
| orbit number at epoch: | 87415 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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