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 23336.79728873 .00011489 00000-0 84690-3 0 9996
2 43803 97.5486 35.1659 0009983 255.6895 104.3222 15.03429628273003
Epoch (UTC): | 02 December 2023 19:08:05 |
Eccentricity: | 0.0009983 |
inclination: | 97.5486° |
perigee height: | 549 km |
apogee height: | 563 km |
right ascension of ascending node: | 35.1659° |
argument of perigee: | 255.6895° |
revolutions per day: | 15.03429628 |
mean anomaly at epoch: | 104.3222° |
orbit number at epoch: | 27300 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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