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 27601U 02056E 21111.83100959 -.00000009 00000-0 11156-4 0 9998
2 27601 98.1947 137.1940 0073403 79.0316 93.4462 14.31990896958824
Epoch (UTC): | 21 April 2021 19:56:39 |
Eccentricity: | 0.0073403 |
inclination: | 98.1947° |
perigee height: | 732 km |
apogee height: | 837 km |
right ascension of ascending node: | 137.1940° |
argument of perigee: | 79.0316° |
revolutions per day: | 14.31990896 |
mean anomaly at epoch: | 93.4462° |
orbit number at epoch: | 95882 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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