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 09662U 77002B 23151.76458688 .00000127 00000-0 75282-4 0 9991
2 09662 81.2731 155.9522 0053231 124.0505 236.5732 14.01035516370843
Epoch (UTC): | 31 May 2023 18:21:00 |
Eccentricity: | 0.0053231 |
inclination: | 81.2731° |
perigee height: | 851 km |
apogee height: | 929 km |
right ascension of ascending node: | 155.9522° |
argument of perigee: | 124.0505° |
revolutions per day: | 14.01035516 |
mean anomaly at epoch: | 236.5732° |
orbit number at epoch: | 37084 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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