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 24259.84808009 .00011352 00000-0 11280-2 0 9995
2 39417 97.7420 213.9108 0047467 217.9892 141.7976 14.91013291585087
Epoch (UTC): | 15 September 2024 20:21:14 |
Eccentricity: | 0.0047467 |
inclination: | 97.7420° |
perigee height: | 561 km |
apogee height: | 628 km |
right ascension of ascending node: | 213.9108° |
argument of perigee: | 217.9892° |
revolutions per day: | 14.91013291 |
mean anomaly at epoch: | 141.7976° |
orbit number at epoch: | 58508 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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