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 40109U 14047A 22178.92692636 -.00000039 00000-0 71320-4 0 9993
2 40109 63.3883 153.4624 0261646 8.2178 352.3006 13.45219812387387
Epoch (UTC): | 27 June 2022 22:14:46 |
Eccentricity: | 0.0261646 |
inclination: | 63.3883° |
perigee height: | 894 km |
apogee height: | 1285 km |
right ascension of ascending node: | 153.4624° |
argument of perigee: | 8.2178° |
revolutions per day: | 13.45219812 |
mean anomaly at epoch: | 352.3006° |
orbit number at epoch: | 38738 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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