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 46U 60007B 22148.08999534 .00000309 00000-0 82607-4 0 9996
2 46 66.6901 288.6961 0214209 320.4889 38.0764 14.49688841241943
Epoch (UTC): | 28 May 2022 02:09:35 |
Eccentricity: | 0.0214209 |
inclination: | 66.6901° |
perigee height: | 574 km |
apogee height: | 879 km |
right ascension of ascending node: | 288.6961° |
argument of perigee: | 320.4889° |
revolutions per day: | 14.49688841 |
mean anomaly at epoch: | 38.0764° |
orbit number at epoch: | 24194 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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