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 24307.43183725 .00010362 00000-0 13223-2 0 9996
2 40043 97.7094 104.4662 0053145 211.9868 147.8115 14.80635196558205
Epoch (UTC): | 02 November 2024 10:21:50 |
Eccentricity: | 0.0053145 |
inclination: | 97.7094° |
perigee height: | 590 km |
apogee height: | 664 km |
right ascension of ascending node: | 104.4662° |
argument of perigee: | 211.9868° |
revolutions per day: | 14.80635196 |
mean anomaly at epoch: | 147.8115° |
orbit number at epoch: | 55820 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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