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 43678U 18084H 23335.92142447 .00003257 00000-0 30945-3 0 9999
2 43678 98.0457 123.6157 0008793 334.9072 25.1718 14.94203051277305
Epoch (UTC): | 01 December 2023 22:06:51 |
Eccentricity: | 0.0008793 |
inclination: | 98.0457° |
perigee height: | 579 km |
apogee height: | 591 km |
right ascension of ascending node: | 123.6157° |
argument of perigee: | 334.9072° |
revolutions per day: | 14.94203051 |
mean anomaly at epoch: | 25.1718° |
orbit number at epoch: | 27730 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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