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 18111.59440202 +.00000289 +00000-0 +17341-3 0 9997
2 23405 070.9818 286.9702 0004241 236.5747 123.4971 14.15199973208891
Epoch (UTC): | 21 April 2018 14:15:56 |
Eccentricity: | 0.0004241 |
inclination: | 70.9818° |
perigee height: | 838 km |
apogee height: | 844 km |
right ascension of ascending node: | 286.9702° |
argument of perigee: | 236.5747° |
revolutions per day: | 14.15199973 |
mean anomaly at epoch: | 123.4971° |
orbit number at epoch: | 20889 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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