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 35946U 09055A 23333.78477737 .00000480 00000-0 17468-3 0 9991
2 35946 98.4360 45.5662 0002210 126.5785 233.5606 14.37549041742103
Epoch (UTC): | 29 November 2023 18:50:04 |
Eccentricity: | 0.0002210 |
inclination: | 98.4360° |
perigee height: | 765 km |
apogee height: | 768 km |
right ascension of ascending node: | 45.5662° |
argument of perigee: | 126.5785° |
revolutions per day: | 14.37549041 |
mean anomaly at epoch: | 233.5606° |
orbit number at epoch: | 74210 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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