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 39417U 13066B 23087.89466413 .00005134 00000-0 60259-3 0 9999
2 39417 97.6773 52.4567 0055114 189.5763 170.4406 14.84262523505288
Epoch (UTC): | 28 March 2023 21:28:18 |
Eccentricity: | 0.0055114 |
inclination: | 97.6773° |
perigee height: | 577 km |
apogee height: | 654 km |
right ascension of ascending node: | 52.4567° |
argument of perigee: | 189.5763° |
revolutions per day: | 14.84262523 |
mean anomaly at epoch: | 170.4406° |
orbit number at epoch: | 50528 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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