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 43803U 18099AX 23333.40281494 .00009930 00000-0 73448-3 0 9991
2 43803 97.5492 31.8563 0009766 268.4396 91.5711 15.03343433272495
Epoch (UTC): | 29 November 2023 09:40:03 |
Eccentricity: | 0.0009766 |
inclination: | 97.5492° |
perigee height: | 550 km |
apogee height: | 563 km |
right ascension of ascending node: | 31.8563° |
argument of perigee: | 268.4396° |
revolutions per day: | 15.03343433 |
mean anomaly at epoch: | 91.5711° |
orbit number at epoch: | 27249 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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