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 23081.15821240 .00001336 00000-0 31134-3 0 9995
2 35935 98.5376 310.7931 0006975 296.1025 63.9454 14.56481157716323
Epoch (UTC): | 22 March 2023 03:47:49 |
Eccentricity: | 0.0006975 |
inclination: | 98.5376° |
perigee height: | 699 km |
apogee height: | 709 km |
right ascension of ascending node: | 310.7931° |
argument of perigee: | 296.1025° |
revolutions per day: | 14.56481157 |
mean anomaly at epoch: | 63.9454° |
orbit number at epoch: | 71632 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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