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 23439U 94085A 23087.55996502 -.00000039 00000-0 10000-3 0 9995
2 23439 64.8146 46.0943 0164994 224.2925 134.4695 11.27574028163523
Epoch (UTC): | 28 March 2023 13:26:20 |
Eccentricity: | 0.0164994 |
inclination: | 64.8146° |
perigee height: | 1884 km |
apogee height: | 2161 km |
right ascension of ascending node: | 46.0943° |
argument of perigee: | 224.2925° |
revolutions per day: | 11.27574028 |
mean anomaly at epoch: | 134.4695° |
orbit number at epoch: | 16352 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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