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 31018U 99025BDL 24357.66072981 .00005263 00000-0 27662-2 0 9999
2 31018 99.0389 73.9670 0059950 51.0408 309.6084 14.13582990910328
Epoch (UTC): | 22 December 2024 15:51:27 |
Eccentricity: | 0.0059950 |
inclination: | 99.0389° |
perigee height: | 804 km |
apogee height: | 890 km |
right ascension of ascending node: | 73.9670° |
argument of perigee: | 51.0408° |
revolutions per day: | 14.13582990 |
mean anomaly at epoch: | 309.6084° |
orbit number at epoch: | 91032 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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