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 16791U 86046A 23151.83910437 .00003795 00000-0 23829-3 0 9996
2 16791 82.4630 69.9954 0020111 241.3327 118.5880 15.08848013 12550
Epoch (UTC): | 31 May 2023 20:08:18 |
Eccentricity: | 0.0020111 |
inclination: | 82.4630° |
perigee height: | 526 km |
apogee height: | 553 km |
right ascension of ascending node: | 69.9954° |
argument of perigee: | 241.3327° |
revolutions per day: | 15.08848013 |
mean anomaly at epoch: | 118.5880° |
orbit number at epoch: | 1255 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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