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 43339U 18036A 23265.49810722 -.00000316 00000-0 00000+0 0 9991
2 43339 0.0140 166.3108 0000009 70.2779 77.9235 1.00269735 8728
Epoch (UTC): | 22 September 2023 11:57:16 |
Eccentricity: | 0.0000009 |
inclination: | 0.0140° |
perigee height: | 35787 km |
apogee height: | 35787 km |
right ascension of ascending node: | 166.3108° |
argument of perigee: | 70.2779° |
revolutions per day: | 1.00269735 |
mean anomaly at epoch: | 77.9235° |
orbit number at epoch: | 872 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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