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 40028U 14033U 23266.78979851 .00007252 00000-0 67727-3 0 9996
2 40028 98.0153 216.9824 0011668 337.7998 22.2714 14.94431698503300
Epoch (UTC): | 23 September 2023 18:57:18 |
Eccentricity: | 0.0011668 |
inclination: | 98.0153° |
perigee height: | 576 km |
apogee height: | 592 km |
right ascension of ascending node: | 216.9824° |
argument of perigee: | 337.7998° |
revolutions per day: | 14.94431698 |
mean anomaly at epoch: | 22.2714° |
orbit number at epoch: | 50330 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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