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 23340.50942588 .00153521 00000-0 13902-2 0 9999
2 39136 64.8561 124.5803 0017912 265.7645 94.1459 15.67143476588380
Epoch (UTC): | 06 December 2023 12:13:34 |
Eccentricity: | 0.0017912 |
inclination: | 64.8561° |
perigee height: | 355 km |
apogee height: | 379 km |
right ascension of ascending node: | 124.5803° |
argument of perigee: | 265.7645° |
revolutions per day: | 15.67143476 |
mean anomaly at epoch: | 94.1459° |
orbit number at epoch: | 58838 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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