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 00053U 60009E 21023.77377164 -.00000103 00000-0 -17251-3 0 9998
2 00053 47.2772 299.5603 0100425 11.9767 348.3379 12.17252491695401
Epoch (UTC): | 23 January 2021 18:34:13 |
Eccentricity: | 0.0100425 |
inclination: | 47.2772° |
perigee height: | 1524 km |
apogee height: | 1684 km |
right ascension of ascending node: | 299.5603° |
argument of perigee: | 11.9767° |
revolutions per day: | 12.17252491 |
mean anomaly at epoch: | 348.3379° |
orbit number at epoch: | 69540 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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