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 23851U 96024A 18108.27351164 0.00000100 00000-0 70433-4 0 02
2 23851 98.6858 102.4143 0007004 204.0457 155.9541 13.98068160 05
| Epoch (UTC): | 18 April 2018 06:33:51 |
| Eccentricity: | 0.0007004 |
| inclination: | 98.6858° |
| perigee height: | 895 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 102.4143° |
| argument of perigee: | 204.0457° |
| revolutions per day: | 13.98068160 |
| mean anomaly at epoch: | 155.9541° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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