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 25399U 98043F 19054.05942261 -.00000001 00000-0 18304-4 0 9992
2 25399 98.6458 356.0936 0000804 313.8027 46.3086 14.24633322 71957
Epoch (UTC): | 23 February 2019 01:25:34 |
Eccentricity: | 0.0000804 |
inclination: | 98.6458° |
perigee height: | 809 km |
apogee height: | 810 km |
right ascension of ascending node: | 356.0936° |
argument of perigee: | 313.8027° |
revolutions per day: | 14.24633322 |
mean anomaly at epoch: | 46.3086° |
orbit number at epoch: | 7195 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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