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 04564U 70079A 21065.84067672 -.00000066 00000-0 19325-4 0 9993
2 04564 65.2765 275.0413 0048335 92.7054 267.9540 13.78442650537417
Epoch (UTC): | 06 March 2021 20:10:34 |
Eccentricity: | 0.0048335 |
inclination: | 65.2765° |
perigee height: | 934 km |
apogee height: | 1005 km |
right ascension of ascending node: | 275.0413° |
argument of perigee: | 92.7054° |
revolutions per day: | 13.78442650 |
mean anomaly at epoch: | 267.9540° |
orbit number at epoch: | 53741 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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