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 37169U 10048B 23151.53817035 .00014165 00000-0 34494-3 0 9997
2 37169 97.9962 357.4694 0005622 83.2858 276.9026 15.41045925704848
Epoch (UTC): | 31 May 2023 12:54:57 |
Eccentricity: | 0.0005622 |
inclination: | 97.9962° |
perigee height: | 439 km |
apogee height: | 447 km |
right ascension of ascending node: | 357.4694° |
argument of perigee: | 83.2858° |
revolutions per day: | 15.41045925 |
mean anomaly at epoch: | 276.9026° |
orbit number at epoch: | 70484 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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