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 21231U 91029B 24357.79029205 .00000092 00000-0 78313-4 0 9992
2 21231 82.9518 234.5378 0036411 116.9864 312.4389 13.76036640691064
Epoch (UTC): | 22 December 2024 18:58:01 |
Eccentricity: | 0.0036411 |
inclination: | 82.9518° |
perigee height: | 951 km |
apogee height: | 1005 km |
right ascension of ascending node: | 234.5378° |
argument of perigee: | 116.9864° |
revolutions per day: | 13.76036640 |
mean anomaly at epoch: | 312.4389° |
orbit number at epoch: | 69106 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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