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 00045U 60007A 21025.63168306 -.00000003 00000-0 26175-4 0 9994
2 00045 66.6944 155.3709 0252397 155.4425 205.8948 14.33703743 97681
Epoch (UTC): | 25 January 2021 15:09:37 |
Eccentricity: | 0.0252397 |
inclination: | 66.6944° |
perigee height: | 599 km |
apogee height: | 960 km |
right ascension of ascending node: | 155.3709° |
argument of perigee: | 155.4425° |
revolutions per day: | 14.33703743 |
mean anomaly at epoch: | 205.8948° |
orbit number at epoch: | 9768 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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