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 42761U 17034D 23277.33675438 .00017474 00000-0 81312-3 0 9996
2 42761 43.0137 226.5156 0010293 92.4116 267.7912 15.19622369348222
Epoch (UTC): | 04 October 2023 08:04:55 |
Eccentricity: | 0.0010293 |
inclination: | 43.0137° |
perigee height: | 500 km |
apogee height: | 514 km |
right ascension of ascending node: | 226.5156° |
argument of perigee: | 92.4116° |
revolutions per day: | 15.19622369 |
mean anomaly at epoch: | 267.7912° |
orbit number at epoch: | 34822 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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