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 42839U 17042Q 24358.02411489 .00017549 00000-0 10829-2 0 9999
2 42839 97.3904 178.7848 0010958 90.0965 270.1520 15.09922916406017
Epoch (UTC): | 23 December 2024 00:34:43 |
Eccentricity: | 0.0010958 |
inclination: | 97.3904° |
perigee height: | 529 km |
apogee height: | 544 km |
right ascension of ascending node: | 178.7848° |
argument of perigee: | 90.0965° |
revolutions per day: | 15.09922916 |
mean anomaly at epoch: | 270.1520° |
orbit number at epoch: | 40601 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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