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 23589U 95027A 19022.68917764 +.00000001 +00000-0 +00000-0 0 9993
2 23589 010.4573 023.7128 0008268 293.5318 099.5732 00.98749558086315
| Epoch (UTC): | 22 January 2019 16:32:24 |
| Eccentricity: | 0.0008268 |
| inclination: | 10.4573° |
| perigee height: | 36183 km |
| apogee height: | 36253 km |
| right ascension of ascending node: | 23.7128° |
| argument of perigee: | 293.5318° |
| revolutions per day: | 0.98749558 |
| mean anomaly at epoch: | 99.5732° |
| orbit number at epoch: | 8631 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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