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 32750U 08014A 22228.92042978 0.00005482 00000-0 19984-3 0 03
2 32750 98.0827 118.9097 0002883 57.3670 302.6619 15.28203087 00
Epoch (UTC): | 16 August 2022 22:05:25 |
Eccentricity: | 0.0002883 |
inclination: | 98.0827° |
perigee height: | 479 km |
apogee height: | 483 km |
right ascension of ascending node: | 118.9097° |
argument of perigee: | 57.3670° |
revolutions per day: | 15.28203087 |
mean anomaly at epoch: | 302.6619° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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