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 39446U 13066AG 24259.83957186 .00011513 00000-0 12298-2 0 9996
2 39446 97.7872 207.7524 0056301 281.8661 77.6245 14.87777203582172
Epoch (UTC): | 15 September 2024 20:08:59 |
Eccentricity: | 0.0056301 |
inclination: | 97.7872° |
perigee height: | 565 km |
apogee height: | 644 km |
right ascension of ascending node: | 207.7524° |
argument of perigee: | 281.8661° |
revolutions per day: | 14.87777203 |
mean anomaly at epoch: | 77.6245° |
orbit number at epoch: | 58217 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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