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 23405U 94077B 22147.05809582 -.00000006 00000-0 21556-4 0 9994
2 23405 70.9836 20.4885 0000852 152.7874 207.3293 14.15255388420593
Epoch (UTC): | 27 May 2022 01:23:39 |
Eccentricity: | 0.0000852 |
inclination: | 70.9836° |
perigee height: | 841 km |
apogee height: | 842 km |
right ascension of ascending node: | 20.4885° |
argument of perigee: | 152.7874° |
revolutions per day: | 14.15255388 |
mean anomaly at epoch: | 207.3293° |
orbit number at epoch: | 42059 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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