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 59U 60013B 19339.82789497 +.00000088 +00000-0 +29555-5 0 9990
2 59 028.2464 137.9453 0189116 092.6191 269.6016 13.52972280920222
Epoch (UTC): | 05 December 2019 19:52:10 |
Eccentricity: | 0.0189116 |
inclination: | 28.2464° |
perigee height: | 920 km |
apogee height: | 1202 km |
right ascension of ascending node: | 137.9453° |
argument of perigee: | 92.6191° |
revolutions per day: | 13.52972280 |
mean anomaly at epoch: | 269.6016° |
orbit number at epoch: | 92022 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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