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 23335.66954594 .00061211 00000-0 10848-2 0 9993
2 42778 97.1320 7.4906 0005369 193.2298 166.8814 15.50046243358566
Epoch (UTC): | 01 December 2023 16:04:08 |
Eccentricity: | 0.0005369 |
inclination: | 97.1320° |
perigee height: | 413 km |
apogee height: | 420 km |
right ascension of ascending node: | 7.4906° |
argument of perigee: | 193.2298° |
revolutions per day: | 15.50046243 |
mean anomaly at epoch: | 166.8814° |
orbit number at epoch: | 35856 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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