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 23439U 94085A 23153.81145634 -.00000055 00000-0 -35235-3 0 9996
2 23439 64.8173 298.9361 0162691 212.7394 146.3363 11.27574241170708
Epoch (UTC): | 02 June 2023 19:28:29 |
Eccentricity: | 0.0162691 |
inclination: | 64.8173° |
perigee height: | 1885 km |
apogee height: | 2159 km |
right ascension of ascending node: | 298.9361° |
argument of perigee: | 212.7394° |
revolutions per day: | 11.27574241 |
mean anomaly at epoch: | 146.3363° |
orbit number at epoch: | 17070 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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