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 36599U 10028B 19341.34718984 -.00000001 00000-0 10487-4 0 9991
2 36599 98.2803 197.9395 0056584 58.2219 302.4489 14.56066355502022
| Epoch (UTC): | 07 December 2019 08:19:57 |
| Eccentricity: | 0.0056584 |
| inclination: | 98.2803° |
| perigee height: | 666 km |
| apogee height: | 746 km |
| right ascension of ascending node: | 197.9395° |
| argument of perigee: | 58.2219° |
| revolutions per day: | 14.56066355 |
| mean anomaly at epoch: | 302.4489° |
| orbit number at epoch: | 50202 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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