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 965U 64083D 23341.60579532 .00000095 00000-0 11920-3 0 9991
2 965 90.0389 197.4017 0043148 95.4576 282.6717 13.56852012919067
Epoch (UTC): | 07 December 2023 14:32:20 |
Eccentricity: | 0.0043148 |
inclination: | 90.0389° |
perigee height: | 1015 km |
apogee height: | 1079 km |
right ascension of ascending node: | 197.4017° |
argument of perigee: | 95.4576° |
revolutions per day: | 13.56852012 |
mean anomaly at epoch: | 282.6717° |
orbit number at epoch: | 91906 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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