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 22176.77544995 .00000816 00000-0 12481-3 0 9994
2 40043 97.6562 5.5865 0060428 128.6632 232.0007 14.75025494430850
Epoch (UTC): | 25 June 2022 18:36:38 |
Eccentricity: | 0.0060428 |
inclination: | 97.6562° |
perigee height: | 602 km |
apogee height: | 687 km |
right ascension of ascending node: | 5.5865° |
argument of perigee: | 128.6632° |
revolutions per day: | 14.75025494 |
mean anomaly at epoch: | 232.0007° |
orbit number at epoch: | 43085 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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