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 27847U 03031H 23335.45920032 .00000695 00000-0 32936-3 0 9992
2 27847 98.6892 339.5218 0008980 343.8988 16.1903 14.22786937 59622
Epoch (UTC): | 01 December 2023 11:01:14 |
Eccentricity: | 0.0008980 |
inclination: | 98.6892° |
perigee height: | 809 km |
apogee height: | 822 km |
right ascension of ascending node: | 339.5218° |
argument of perigee: | 343.8988° |
revolutions per day: | 14.22786937 |
mean anomaly at epoch: | 16.1903° |
orbit number at epoch: | 5962 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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