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 22180.50648023 .00000582 00000-0 91115-4 0 9999
2 40043 97.6560 9.1160 0060596 116.8283 243.9140 14.75031310431408
Epoch (UTC): | 29 June 2022 12:09:19 |
Eccentricity: | 0.0060596 |
inclination: | 97.6560° |
perigee height: | 602 km |
apogee height: | 687 km |
right ascension of ascending node: | 9.1160° |
argument of perigee: | 116.8283° |
revolutions per day: | 14.75031310 |
mean anomaly at epoch: | 243.9140° |
orbit number at epoch: | 43140 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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