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 26960U 01049D 21062.73285572 .00000795 00000-0 53726-4 0 9995
2 26960 97.8246 66.5474 0052792 238.5830 121.0229 15.08589660 58320
Epoch (UTC): | 03 March 2021 17:35:18 |
Eccentricity: | 0.0052792 |
inclination: | 97.8246° |
perigee height: | 504 km |
apogee height: | 577 km |
right ascension of ascending node: | 66.5474° |
argument of perigee: | 238.5830° |
revolutions per day: | 15.08589660 |
mean anomaly at epoch: | 121.0229° |
orbit number at epoch: | 5832 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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