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 25489U 98055A 23081.69851344 .00000848 00000-0 21660-3 0 9997
2 25489 84.9844 321.2809 0009460 3.5331 356.5936 14.49353994292254
Epoch (UTC): | 22 March 2023 16:45:51 |
Eccentricity: | 0.0009460 |
inclination: | 84.9844° |
perigee height: | 721 km |
apogee height: | 734 km |
right ascension of ascending node: | 321.2809° |
argument of perigee: | 3.5331° |
revolutions per day: | 14.49353994 |
mean anomaly at epoch: | 356.5936° |
orbit number at epoch: | 29225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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