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 39092U 13009G 18110.82472014 -.00000002 +00000-0 +14720-4 0 9996
2 39092 098.5258 316.8991 0010534 106.7435 253.4907 14.34941671269588
Epoch (UTC): | 20 April 2018 19:47:35 |
Eccentricity: | 0.0010534 |
inclination: | 98.5258° |
perigee height: | 768 km |
apogee height: | 783 km |
right ascension of ascending node: | 316.8991° |
argument of perigee: | 106.7435° |
revolutions per day: | 14.34941671 |
mean anomaly at epoch: | 253.4907° |
orbit number at epoch: | 26958 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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