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 04420U 70047B 21058.51601616 -.00000123 00000-0 -71209-4 0 9991
2 04420 81.2274 91.2817 0087486 7.4889 352.7565 14.12092926608792
Epoch (UTC): | 27 February 2021 12:23:03 |
Eccentricity: | 0.0087486 |
inclination: | 81.2274° |
perigee height: | 789 km |
apogee height: | 915 km |
right ascension of ascending node: | 91.2817° |
argument of perigee: | 7.4889° |
revolutions per day: | 14.12092926 |
mean anomaly at epoch: | 352.7565° |
orbit number at epoch: | 60879 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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