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 42761U 17034D 23085.84540043 .00013420 00000-0 69874-3 0 9998
2 42761 43.0165 211.4629 0012353 290.9106 207.6783 15.15840183319144
Epoch (UTC): | 26 March 2023 20:17:22 |
Eccentricity: | 0.0012353 |
inclination: | 43.0165° |
perigee height: | 510 km |
apogee height: | 527 km |
right ascension of ascending node: | 211.4629° |
argument of perigee: | 290.9106° |
revolutions per day: | 15.15840183 |
mean anomaly at epoch: | 207.6783° |
orbit number at epoch: | 31914 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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