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 28352U 04021A 23033.49899261 .00000407 00000-0 24877-3 0 9998
2 28352 71.0036 150.6616 0016695 244.8357 115.1033 14.11770255961007
Epoch (UTC): | 02 February 2023 11:58:32 |
Eccentricity: | 0.0016695 |
inclination: | 71.0036° |
perigee height: | 841 km |
apogee height: | 865 km |
right ascension of ascending node: | 150.6616° |
argument of perigee: | 244.8357° |
revolutions per day: | 14.11770255 |
mean anomaly at epoch: | 115.1033° |
orbit number at epoch: | 96100 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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