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 43439U 18040A 22179.63016573 .00005368 00000-0 24024-3 0 9995
2 43439 97.2414 238.1092 0012760 8.0621 114.4787 15.21617305231403
Epoch (UTC): | 28 June 2022 15:07:26 |
Eccentricity: | 0.0012760 |
inclination: | 97.2414° |
perigee height: | 492 km |
apogee height: | 510 km |
right ascension of ascending node: | 238.1092° |
argument of perigee: | 8.0621° |
revolutions per day: | 15.21617305 |
mean anomaly at epoch: | 114.4787° |
orbit number at epoch: | 23140 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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