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 22178.69373118 .00001166 00000-0 10581-3 0 9995
2 43803 97.6197 245.4606 0013478 229.4846 130.5203 14.97127836194606
Epoch (UTC): | 27 June 2022 16:38:58 |
Eccentricity: | 0.0013478 |
inclination: | 97.6197° |
perigee height: | 566 km |
apogee height: | 585 km |
right ascension of ascending node: | 245.4606° |
argument of perigee: | 229.4846° |
revolutions per day: | 14.97127836 |
mean anomaly at epoch: | 130.5203° |
orbit number at epoch: | 19460 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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