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 37769U 11039E 23038.25805906 .00010826 00000-0 17910-2 0 9994
2 37769 98.3837 302.7732 0075437 149.2835 327.9561 14.68610229614063
Epoch (UTC): | 07 February 2023 06:11:36 |
Eccentricity: | 0.0075437 |
inclination: | 98.3837° |
perigee height: | 612 km |
apogee height: | 718 km |
right ascension of ascending node: | 302.7732° |
argument of perigee: | 149.2835° |
revolutions per day: | 14.68610229 |
mean anomaly at epoch: | 327.9561° |
orbit number at epoch: | 61406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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