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 22184.87790878 .00001513 00000-0 99196-4 0 9994
2 42761 43.0174 240.9358 0009160 25.4208 143.6875 15.12093120278846
Epoch (UTC): | 03 July 2022 21:04:11 |
Eccentricity: | 0.0009160 |
inclination: | 43.0174° |
perigee height: | 523 km |
apogee height: | 536 km |
right ascension of ascending node: | 240.9358° |
argument of perigee: | 25.4208° |
revolutions per day: | 15.12093120 |
mean anomaly at epoch: | 143.6875° |
orbit number at epoch: | 27884 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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