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 42788U 17036Z 23278.90222119 .18188609 24489-5 22826-3 0 9990
2 42788 97.0954 322.8452 0011132 248.8258 111.1858 16.49176567350708
Epoch (UTC): | 05 October 2023 21:39:11 |
Eccentricity: | 0.0011132 |
inclination: | 97.0954° |
perigee height: | 134 km |
apogee height: | 149 km |
right ascension of ascending node: | 322.8452° |
argument of perigee: | 248.8258° |
revolutions per day: | 16.49176567 |
mean anomaly at epoch: | 111.1858° |
orbit number at epoch: | 35070 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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