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 24261.58844293 .00082314 00000-0 24551-2 0 9990
2 42761 43.0191 60.8974 0013348 266.4351 93.4977 15.33607873401568
Epoch (UTC): | 17 September 2024 14:07:21 |
Eccentricity: | 0.0013348 |
inclination: | 43.0191° |
perigee height: | 456 km |
apogee height: | 474 km |
right ascension of ascending node: | 60.8974° |
argument of perigee: | 266.4351° |
revolutions per day: | 15.33607873 |
mean anomaly at epoch: | 93.4977° |
orbit number at epoch: | 40156 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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