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 23080.12772879 .00001282 00000-0 29927-3 0 9991
2 35935 98.5378 309.7382 0007003 299.7252 60.3248 14.56477921716176
Epoch (UTC): | 21 March 2023 03:03:55 |
Eccentricity: | 0.0007003 |
inclination: | 98.5378° |
perigee height: | 699 km |
apogee height: | 709 km |
right ascension of ascending node: | 309.7382° |
argument of perigee: | 299.7252° |
revolutions per day: | 14.56477921 |
mean anomaly at epoch: | 60.3248° |
orbit number at epoch: | 71617 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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