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 23335.72094517 .00230822 00000-0 22142-2 0 9993
2 39136 64.8566 141.2244 0018542 260.1513 99.7543 15.65450654588116
Epoch (UTC): | 01 December 2023 17:18:09 |
Eccentricity: | 0.0018542 |
inclination: | 64.8566° |
perigee height: | 359 km |
apogee height: | 384 km |
right ascension of ascending node: | 141.2244° |
argument of perigee: | 260.1513° |
revolutions per day: | 15.65450654 |
mean anomaly at epoch: | 99.7543° |
orbit number at epoch: | 58811 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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