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 00047U 60007C 23036.92239054 .00000662 00000-0 16865-3 0 9995
2 00047 66.6651 98.2200 0231707 316.9368 41.3805 14.42588756273610
Epoch (UTC): | 05 February 2023 22:08:14 |
Eccentricity: | 0.0231707 |
inclination: | 66.6651° |
perigee height: | 585 km |
apogee height: | 915 km |
right ascension of ascending node: | 98.2200° |
argument of perigee: | 316.9368° |
revolutions per day: | 14.42588756 |
mean anomaly at epoch: | 41.3805° |
orbit number at epoch: | 27361 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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