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 5U 58002B 23342.91914036 .00000256 00000-0 31485-3 0 9994
2 5 34.2564 276.7604 1842679 306.1649 38.1895 10.85129860343238
Epoch (UTC): | 08 December 2023 22:03:33 |
Eccentricity: | 0.1842679 |
inclination: | 34.2564° |
perigee height: | 652 km |
apogee height: | 3828 km |
right ascension of ascending node: | 276.7604° |
argument of perigee: | 306.1649° |
revolutions per day: | 10.85129860 |
mean anomaly at epoch: | 38.1895° |
orbit number at epoch: | 34323 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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