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 24954U 97052B 23160.57939678 .00000109 00000-0 89688-4 0 9996
2 24954 82.9227 91.3343 0039433 174.2907 358.9072 13.80115196294768
Epoch (UTC): | 09 June 2023 13:54:19 |
Eccentricity: | 0.0039433 |
inclination: | 82.9227° |
perigee height: | 934 km |
apogee height: | 992 km |
right ascension of ascending node: | 91.3343° |
argument of perigee: | 174.2907° |
revolutions per day: | 13.80115196 |
mean anomaly at epoch: | 358.9072° |
orbit number at epoch: | 29476 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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