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 23657U 95046A 19078.60957410 +.00000166 +00000-0 +16081-4 0 9997
2 23657 082.5297 019.0735 0023483 119.6353 240.7206 14.86043973272277
| Epoch (UTC): | 19 March 2019 14:37:47 |
| Eccentricity: | 0.0023483 |
| inclination: | 82.5297° |
| perigee height: | 594 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 19.0735° |
| argument of perigee: | 119.6353° |
| revolutions per day: | 14.86043973 |
| mean anomaly at epoch: | 240.7206° |
| orbit number at epoch: | 27227 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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