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 23155.89147209 .00000330 00000-0 19711-3 0 9991
2 17973 70.8997 1.4246 0029178 97.5164 262.9273 14.14226805860946
Epoch (UTC): | 04 June 2023 21:23:43 |
Eccentricity: | 0.0029178 |
inclination: | 70.8997° |
perigee height: | 824 km |
apogee height: | 866 km |
right ascension of ascending node: | 1.4246° |
argument of perigee: | 97.5164° |
revolutions per day: | 14.14226805 |
mean anomaly at epoch: | 262.9273° |
orbit number at epoch: | 86094 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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