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 40045U 14033AM 23336.49310958 .00020706 00000-0 26352-2 0 9995
2 40045 97.6575 153.3796 0052241 208.3319 151.5051 14.80616026508519
Epoch (UTC): | 02 December 2023 11:50:04 |
Eccentricity: | 0.0052241 |
inclination: | 97.6575° |
perigee height: | 591 km |
apogee height: | 664 km |
right ascension of ascending node: | 153.3796° |
argument of perigee: | 208.3319° |
revolutions per day: | 14.80616026 |
mean anomaly at epoch: | 151.5051° |
orbit number at epoch: | 50851 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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