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 28931U 06002A 21064.17622184 .00000180 00000-0 43977-4 0 9998
2 28931 97.8748 43.5476 0001876 35.2799 324.8523 14.62805100805810
Epoch (UTC): | 05 March 2021 04:13:45 |
Eccentricity: | 0.0001876 |
inclination: | 97.8748° |
perigee height: | 683 km |
apogee height: | 685 km |
right ascension of ascending node: | 43.5476° |
argument of perigee: | 35.2799° |
revolutions per day: | 14.62805100 |
mean anomaly at epoch: | 324.8523° |
orbit number at epoch: | 80581 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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