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 17070U 86088A 23088.41904736 .00000213 00000-0 21085-3 0 9995
2 17070 89.5807 224.7569 0037970 222.1170 198.1333 13.74927549823833
Epoch (UTC): | 29 March 2023 10:03:25 |
Eccentricity: | 0.0037970 |
inclination: | 89.5807° |
perigee height: | 954 km |
apogee height: | 1010 km |
right ascension of ascending node: | 224.7569° |
argument of perigee: | 222.1170° |
revolutions per day: | 13.74927549 |
mean anomaly at epoch: | 198.1333° |
orbit number at epoch: | 82383 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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