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 36566U 97051WV 23336.41146021 .00206713 00000-0 54702-1 0 9992
2 36566 86.4242 136.5639 0121023 93.6795 267.8254 14.43229911739082
Epoch (UTC): | 02 December 2023 09:52:30 |
Eccentricity: | 0.0121023 |
inclination: | 86.4242° |
perigee height: | 661 km |
apogee height: | 834 km |
right ascension of ascending node: | 136.5639° |
argument of perigee: | 93.6795° |
revolutions per day: | 14.43229911 |
mean anomaly at epoch: | 267.8254° |
orbit number at epoch: | 73908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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