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 23333.64362594 .00002270 00000-0 51424-3 0 9993
2 35935 98.4975 208.7822 0006844 231.0171 129.0418 14.57119308753082
Epoch (UTC): | 29 November 2023 15:26:49 |
Eccentricity: | 0.0006844 |
inclination: | 98.4975° |
perigee height: | 697 km |
apogee height: | 707 km |
right ascension of ascending node: | 208.7822° |
argument of perigee: | 231.0171° |
revolutions per day: | 14.57119308 |
mean anomaly at epoch: | 129.0418° |
orbit number at epoch: | 75308 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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