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 24971U 97057A 24306.51973172 .00001151 00000-0 41358-3 0 9993
2 24971 98.7818 277.1332 0052538 172.0473 188.1556 14.35003718417590
Epoch (UTC): | 01 November 2024 12:28:24 |
Eccentricity: | 0.0052538 |
inclination: | 98.7818° |
perigee height: | 737 km |
apogee height: | 812 km |
right ascension of ascending node: | 277.1332° |
argument of perigee: | 172.0473° |
revolutions per day: | 14.35003718 |
mean anomaly at epoch: | 188.1556° |
orbit number at epoch: | 41759 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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