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 38857U 12055A 23026.19333641 -.00000003 00000-0 00000-0 0 9991
2 38857 55.2067 135.5736 0003096 241.6810 118.2770 1.70473578 63904
Epoch (UTC): | 26 January 2023 04:38:24 |
Eccentricity: | 0.0003096 |
inclination: | 55.2067° |
perigee height: | 23213 km |
apogee height: | 23231 km |
right ascension of ascending node: | 135.5736° |
argument of perigee: | 241.6810° |
revolutions per day: | 1.70473578 |
mean anomaly at epoch: | 118.2770° |
orbit number at epoch: | 6390 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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