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 32788U 08021F 21016.06769424 .00000781 00000-0 75612-4 0 9998
2 32788 97.4974 17.2072 0013057 65.2484 295.0094 14.95345281691180
Epoch (UTC): | 16 January 2021 01:37:28 |
Eccentricity: | 0.0013057 |
inclination: | 97.4974° |
perigee height: | 572 km |
apogee height: | 590 km |
right ascension of ascending node: | 17.2072° |
argument of perigee: | 65.2484° |
revolutions per day: | 14.95345281 |
mean anomaly at epoch: | 295.0094° |
orbit number at epoch: | 69118 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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