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 40043U 14033AK 22178.47137481 .00000824 00000-0 12606-3 0 9999
2 40043 97.6561 7.1909 0060495 123.2823 237.4203 14.75029057431108
Epoch (UTC): | 27 June 2022 11:18:46 |
Eccentricity: | 0.0060495 |
inclination: | 97.6561° |
perigee height: | 602 km |
apogee height: | 687 km |
right ascension of ascending node: | 7.1909° |
argument of perigee: | 123.2823° |
revolutions per day: | 14.75029057 |
mean anomaly at epoch: | 237.4203° |
orbit number at epoch: | 43110 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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