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 21061.44010727 .00000196 00000-0 47035-4 0 9995
2 28931 97.8742 40.9360 0002005 39.1609 320.9730 14.62804012805419
Epoch (UTC): | 02 March 2021 10:33:45 |
Eccentricity: | 0.0002005 |
inclination: | 97.8742° |
perigee height: | 683 km |
apogee height: | 685 km |
right ascension of ascending node: | 40.9360° |
argument of perigee: | 39.1609° |
revolutions per day: | 14.62804012 |
mean anomaly at epoch: | 320.9730° |
orbit number at epoch: | 80541 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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