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 39136U 13015G 23333.48440082 .00162433 00000-0 16239-2 0 9998
2 39136 64.8561 148.9804 0018850 258.5945 101.3087 15.64622409587760
Epoch (UTC): | 29 November 2023 11:37:32 |
Eccentricity: | 0.0018850 |
inclination: | 64.8561° |
perigee height: | 361 km |
apogee height: | 387 km |
right ascension of ascending node: | 148.9804° |
argument of perigee: | 258.5945° |
revolutions per day: | 15.64622409 |
mean anomaly at epoch: | 101.3087° |
orbit number at epoch: | 58776 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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