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 6173U 72069A 23083.27698913 .00003857 00000-0 97976-3 0 9996
2 6173 89.9643 209.8439 0054430 113.3543 313.1597 14.49745404659527
Epoch (UTC): | 24 March 2023 06:38:51 |
Eccentricity: | 0.0054430 |
inclination: | 89.9643° |
perigee height: | 688 km |
apogee height: | 765 km |
right ascension of ascending node: | 209.8439° |
argument of perigee: | 113.3543° |
revolutions per day: | 14.49745404 |
mean anomaly at epoch: | 313.1597° |
orbit number at epoch: | 65952 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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