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 43156U 18008B 24198.66905212 .17296646 24655-5 28398-3 0 9992
2 43156 97.2151 256.8209 0016593 258.3712 101.5729 16.46899832359648
Epoch (UTC): | 16 July 2024 16:03:26 |
Eccentricity: | 0.0016593 |
inclination: | 97.2151° |
perigee height: | 136 km |
apogee height: | 158 km |
right ascension of ascending node: | 256.8209° |
argument of perigee: | 258.3712° |
revolutions per day: | 16.46899832 |
mean anomaly at epoch: | 101.5729° |
orbit number at epoch: | 35964 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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