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 30775U 07006D 23088.48718524 .00058564 00000-0 10755-2 0 9993
2 30775 35.4476 119.8369 0004789 178.5814 181.4931 15.48123480890978
Epoch (UTC): | 29 March 2023 11:41:32 |
Eccentricity: | 0.0004789 |
inclination: | 35.4476° |
perigee height: | 419 km |
apogee height: | 425 km |
right ascension of ascending node: | 119.8369° |
argument of perigee: | 178.5814° |
revolutions per day: | 15.48123480 |
mean anomaly at epoch: | 181.4931° |
orbit number at epoch: | 89097 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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