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 23335.15433898 .00001986 00000-0 45122-3 0 9998
2 35935 98.4972 210.3236 0006926 225.6529 134.4102 14.57124766753303
Epoch (UTC): | 01 December 2023 03:42:14 |
Eccentricity: | 0.0006926 |
inclination: | 98.4972° |
perigee height: | 697 km |
apogee height: | 707 km |
right ascension of ascending node: | 210.3236° |
argument of perigee: | 225.6529° |
revolutions per day: | 14.57124766 |
mean anomaly at epoch: | 134.4102° |
orbit number at epoch: | 75330 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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