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 39440U 13066AA 22141.89836292 .00002614 00000-0 36054-3 0 9997
2 39440 97.7239 100.5773 0077731 216.6899 142.8976 14.76935010456365
Epoch (UTC): | 21 May 2022 21:33:38 |
Eccentricity: | 0.0077731 |
inclination: | 97.7239° |
perigee height: | 584 km |
apogee height: | 693 km |
right ascension of ascending node: | 100.5773° |
argument of perigee: | 216.6899° |
revolutions per day: | 14.76935010 |
mean anomaly at epoch: | 142.8976° |
orbit number at epoch: | 45636 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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