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 25544U 98067A 19349.15475490 .00016717 00000-0 10270-3 0 9042
2 25544 51.6380 184.1461 0007489 35.7278 324.4373 15.50109295 3321
Epoch (UTC): | 15 December 2019 03:42:50 |
Eccentricity: | 0.0007489 |
inclination: | 51.6380° |
perigee height: | 411 km |
apogee height: | 421 km |
right ascension of ascending node: | 184.1461° |
argument of perigee: | 35.7278° |
revolutions per day: | 15.50109295 |
mean anomaly at epoch: | 324.4373° |
orbit number at epoch: | 332 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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