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 29092U 06015A 21101.79228403 .00000103 00000-0 19075-4 0 9994
2 29092 97.9149 129.8164 0001422 90.9953 269.1424 14.83145868808954
Epoch (UTC): | 11 April 2021 19:00:53 |
Eccentricity: | 0.0001422 |
inclination: | 97.9149° |
perigee height: | 618 km |
apogee height: | 620 km |
right ascension of ascending node: | 129.8164° |
argument of perigee: | 90.9953° |
revolutions per day: | 14.83145868 |
mean anomaly at epoch: | 269.1424° |
orbit number at epoch: | 80895 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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