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 33498U 09002G 19348.83444220 .00000158 00000-0 28887-4 0 9991
2 33498 98.2851 203.6253 0010157 319.6198 40.4257 14.79064160586485
| Epoch (UTC): | 14 December 2019 20:01:35 |
| Eccentricity: | 0.0010157 |
| inclination: | 98.2851° |
| perigee height: | 625 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 203.6253° |
| argument of perigee: | 319.6198° |
| revolutions per day: | 14.79064160 |
| mean anomaly at epoch: | 40.4257° |
| orbit number at epoch: | 58648 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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