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 15517U 85013B 23153.51557190 .00000041 00000-0 23249-4 0 9992
2 15517 82.5340 148.3181 0014390 194.5420 165.5328 13.84924206936277
Epoch (UTC): | 02 June 2023 12:22:25 |
Eccentricity: | 0.0014390 |
inclination: | 82.5340° |
perigee height: | 936 km |
apogee height: | 957 km |
right ascension of ascending node: | 148.3181° |
argument of perigee: | 194.5420° |
revolutions per day: | 13.84924206 |
mean anomaly at epoch: | 165.5328° |
orbit number at epoch: | 93627 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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