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 39439U 13066Z 22179.19353006 .00002541 00000-0 29888-3 0 9992
2 39439 97.6369 152.5867 0063077 6.4940 353.7078 14.84286823464733
Epoch (UTC): | 28 June 2022 04:38:40 |
Eccentricity: | 0.0063077 |
inclination: | 97.6369° |
perigee height: | 572 km |
apogee height: | 660 km |
right ascension of ascending node: | 152.5867° |
argument of perigee: | 6.4940° |
revolutions per day: | 14.84286823 |
mean anomaly at epoch: | 353.7078° |
orbit number at epoch: | 46473 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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