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 39026U 12072A 19343.53290810 .00000627 00000-0 25026-4 0 9994
2 39026 97.2159 341.1407 0036996 200.7682 159.2057 15.28226298388141
Epoch (UTC): | 09 December 2019 12:47:23 |
Eccentricity: | 0.0036996 |
inclination: | 97.2159° |
perigee height: | 456 km |
apogee height: | 506 km |
right ascension of ascending node: | 341.1407° |
argument of perigee: | 200.7682° |
revolutions per day: | 15.28226298 |
mean anomaly at epoch: | 159.2057° |
orbit number at epoch: | 38814 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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