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 23332.13816154 .00009703 00000-0 71829-3 0 9996
2 43803 97.5499 30.6228 0009595 272.7558 87.2569 15.03317328272302
Epoch (UTC): | 28 November 2023 03:18:57 |
Eccentricity: | 0.0009595 |
inclination: | 97.5499° |
perigee height: | 550 km |
apogee height: | 563 km |
right ascension of ascending node: | 30.6228° |
argument of perigee: | 272.7558° |
revolutions per day: | 15.03317328 |
mean anomaly at epoch: | 87.2569° |
orbit number at epoch: | 27230 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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