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 40912U 15049P 19052.01542839 .00000898 00000-0 45697-4 0 9994
2 40912 97.4499 60.9096 0013817 218.5354 197.4589 15.19317825189449
Epoch (UTC): | 21 February 2019 00:22:13 |
Eccentricity: | 0.0013817 |
inclination: | 97.4499° |
perigee height: | 498 km |
apogee height: | 517 km |
right ascension of ascending node: | 60.9096° |
argument of perigee: | 218.5354° |
revolutions per day: | 15.19317825 |
mean anomaly at epoch: | 197.4589° |
orbit number at epoch: | 18944 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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