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 43143U 18004AJ 23316.95209561 .02592973 24144-5 77798-3 0 9998
2 43143 97.3097 50.6433 0009283 280.2242 79.8004 16.26944402326103
Epoch (UTC): | 12 November 2023 22:51:01 |
Eccentricity: | 0.0009283 |
inclination: | 97.3097° |
perigee height: | 194 km |
apogee height: | 207 km |
right ascension of ascending node: | 50.6433° |
argument of perigee: | 280.2242° |
revolutions per day: | 16.26944402 |
mean anomaly at epoch: | 79.8004° |
orbit number at epoch: | 32610 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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