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 17973U 87041A 23156.59878063 .00000317 00000-0 19034-3 0 9991
2 17973 70.8997 359.9335 0029164 96.3765 264.0680 14.14227325861040
Epoch (UTC): | 05 June 2023 14:22:14 |
Eccentricity: | 0.0029164 |
inclination: | 70.8997° |
perigee height: | 824 km |
apogee height: | 866 km |
right ascension of ascending node: | 359.9335° |
argument of perigee: | 96.3765° |
revolutions per day: | 14.14227325 |
mean anomaly at epoch: | 264.0680° |
orbit number at epoch: | 86104 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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