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 42778U 17036P 23341.54308237 .00028975 00000-0 50680-3 0 9993
2 42778 97.1333 13.3056 0006052 172.0022 188.1328 15.50575443359479
Epoch (UTC): | 07 December 2023 13:02:02 |
Eccentricity: | 0.0006052 |
inclination: | 97.1333° |
perigee height: | 411 km |
apogee height: | 419 km |
right ascension of ascending node: | 13.3056° |
argument of perigee: | 172.0022° |
revolutions per day: | 15.50575443 |
mean anomaly at epoch: | 188.1328° |
orbit number at epoch: | 35947 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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