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 60235U 24128A 24316.21771115 .00008271 00000-0 73443-3 0 9996
2 60235 61.9952 92.7150 0027283 344.4837 15.5411 14.96547476 18604
Epoch (UTC): | 11 November 2024 05:13:30 |
Eccentricity: | 0.0027283 |
inclination: | 61.9952° |
perigee height: | 558 km |
apogee height: | 596 km |
right ascension of ascending node: | 92.7150° |
argument of perigee: | 344.4837° |
revolutions per day: | 14.96547476 |
mean anomaly at epoch: | 15.5411° |
orbit number at epoch: | 1860 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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