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 23711U 95059B 23159.49303497 -.00000047 00000-0 -76924-5 0 9997
2 23711 100.5949 179.0194 0368530 74.4329 47.6517 13.12762028321951
Epoch (UTC): | 08 June 2023 11:49:58 |
Eccentricity: | 0.0368530 |
inclination: | 100.5949° |
perigee height: | 933 km |
apogee height: | 1492 km |
right ascension of ascending node: | 179.0194° |
argument of perigee: | 74.4329° |
revolutions per day: | 13.12762028 |
mean anomaly at epoch: | 47.6517° |
orbit number at epoch: | 32195 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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