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 34638U 93036XK 23336.44025146 .00147273 00000-0 20765-1 0 9993
2 34638 74.0377 331.3985 0010442 237.4956 241.7437 14.76296905780106
Epoch (UTC): | 02 December 2023 10:33:57 |
Eccentricity: | 0.0010442 |
inclination: | 74.0377° |
perigee height: | 634 km |
apogee height: | 648 km |
right ascension of ascending node: | 331.3985° |
argument of perigee: | 237.4956° |
revolutions per day: | 14.76296905 |
mean anomaly at epoch: | 241.7437° |
orbit number at epoch: | 78010 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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