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 18308.15956161 0.00000000 00000-0 00000-0 0 07
2 23851 98.6948 291.7697 0006004 23.7340 336.2659 13.98069246 07
| Epoch (UTC): | 04 November 2018 03:49:46 |
| Eccentricity: | 0.0006004 |
| inclination: | 98.6948° |
| perigee height: | 896 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 291.7697° |
| argument of perigee: | 23.7340° |
| revolutions per day: | 13.98069246 |
| mean anomaly at epoch: | 336.2659° |
| 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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