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 07298U 74033A 23088.71638793 -.00000197 00000-0 00000-0 0 9996
2 07298 7.1524 273.8289 0015757 43.9294 124.0511 0.98614805108297
Epoch (UTC): | 29 March 2023 17:11:35 |
Eccentricity: | 0.0015757 |
inclination: | 7.1524° |
perigee height: | 36190 km |
apogee height: | 36324 km |
right ascension of ascending node: | 273.8289° |
argument of perigee: | 43.9294° |
revolutions per day: | 0.98614805 |
mean anomaly at epoch: | 124.0511° |
orbit number at epoch: | 10829 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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