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 28738U 05024B 22140.44623807 .00006024 00000-0 33818-3 0 9990
2 28738 97.3518 149.5359 0009580 274.7545 85.2593 15.13656785927530
Epoch (UTC): | 20 May 2022 10:42:34 |
Eccentricity: | 0.0009580 |
inclination: | 97.3518° |
perigee height: | 518 km |
apogee height: | 531 km |
right ascension of ascending node: | 149.5359° |
argument of perigee: | 274.7545° |
revolutions per day: | 15.13656785 |
mean anomaly at epoch: | 85.2593° |
orbit number at epoch: | 92753 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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