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 00085U 61004C 21106.51506243 -.00000852 00000-0 -15389-3 0 9996
2 00085 38.7781 273.6115 0388718 359.9541 0.1122 14.21633910974225
Epoch (UTC): | 16 April 2021 12:21:41 |
Eccentricity: | 0.0388718 |
inclination: | 38.7781° |
perigee height: | 540 km |
apogee height: | 1099 km |
right ascension of ascending node: | 273.6115° |
argument of perigee: | 359.9541° |
revolutions per day: | 14.21633910 |
mean anomaly at epoch: | 0.1122° |
orbit number at epoch: | 97422 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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