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 35935U 09051E 24340.24656913 .00002814 00000-0 61248-3 0 9998
2 35935 98.4506 227.2362 0007755 160.8439 199.3053 14.58770672807190
Epoch (UTC): | 05 December 2024 05:55:03 |
Eccentricity: | 0.0007755 |
inclination: | 98.4506° |
perigee height: | 691 km |
apogee height: | 702 km |
right ascension of ascending node: | 227.2362° |
argument of perigee: | 160.8439° |
revolutions per day: | 14.58770672 |
mean anomaly at epoch: | 199.3053° |
orbit number at epoch: | 80719 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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