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 42844U 17042V 21023.60664012 .00000560 00000-0 59689-4 0 9991
2 42844 97.4936 262.7368 0010881 255.2377 104.7637 14.92487753192230
Epoch (UTC): | 23 January 2021 14:33:33 |
Eccentricity: | 0.0010881 |
inclination: | 97.4936° |
perigee height: | 582 km |
apogee height: | 598 km |
right ascension of ascending node: | 262.7368° |
argument of perigee: | 255.2377° |
revolutions per day: | 14.92487753 |
mean anomaly at epoch: | 104.7637° |
orbit number at epoch: | 19223 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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