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 23341.40313212 .00000963 00000-0 22413-3 0 9992
2 35935 98.4976 216.6984 0007218 204.2442 155.8416 14.57143956754182
Epoch (UTC): | 07 December 2023 09:40:30 |
Eccentricity: | 0.0007218 |
inclination: | 98.4976° |
perigee height: | 697 km |
apogee height: | 707 km |
right ascension of ascending node: | 216.6984° |
argument of perigee: | 204.2442° |
revolutions per day: | 14.57143956 |
mean anomaly at epoch: | 155.8416° |
orbit number at epoch: | 75418 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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