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 23465U 95002C 19083.20456772 .00000043 00000-0 31287-4 0 9992
2 23465 82.9305 174.4480 0036172 298.2900 122.1192 13.71887380209843
| Epoch (UTC): | 24 March 2019 04:54:34 |
| Eccentricity: | 0.0036172 |
| inclination: | 82.9305° |
| perigee height: | 966 km |
| apogee height: | 1019 km |
| right ascension of ascending node: | 174.4480° |
| argument of perigee: | 298.2900° |
| revolutions per day: | 13.71887380 |
| mean anomaly at epoch: | 122.1192° |
| orbit number at epoch: | 20984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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