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 32376U 07059A 21016.50725119 -.00000149 00000-0 -12153-4 0 9994
2 32376 97.8824 202.5733 0001340 87.2021 272.9348 14.82157312709130
Epoch (UTC): | 16 January 2021 12:10:26 |
Eccentricity: | 0.0001340 |
inclination: | 97.8824° |
perigee height: | 621 km |
apogee height: | 623 km |
right ascension of ascending node: | 202.5733° |
argument of perigee: | 87.2021° |
revolutions per day: | 14.82157312 |
mean anomaly at epoch: | 272.9348° |
orbit number at epoch: | 70913 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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