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 43446U 18036F 23277.58015429 -.00000240 00000-0 00000-0 0 9991
2 43446 4.6870 78.3524 0009455 125.9716 110.1079 1.02123089 16845
Epoch (UTC): | 04 October 2023 13:55:25 |
Eccentricity: | 0.0009455 |
inclination: | 4.6870° |
perigee height: | 35236 km |
apogee height: | 35314 km |
right ascension of ascending node: | 78.3524° |
argument of perigee: | 125.9716° |
revolutions per day: | 1.02123089 |
mean anomaly at epoch: | 110.1079° |
orbit number at epoch: | 1684 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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