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 13120U 82027A 17351.57038251 .10847703 -90242-6 12875-3 0 9994
2 13120 81.1663 271.5831 0008003 222.8648 137.7432 16.49812145962829
Epoch (UTC): | 17 December 2017 13:41:21 |
Eccentricity: | 0.0008003 |
inclination: | 81.1663° |
perigee height: | 134 km |
apogee height: | 145 km |
right ascension of ascending node: | 271.5831° |
argument of perigee: | 222.8648° |
revolutions per day: | 16.49812145 |
mean anomaly at epoch: | 137.7432° |
orbit number at epoch: | 96282 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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