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 19120U 88039B 23160.92455109 -.00000112 00000-0 -30504-4 0 9990
2 19120 71.0157 30.5070 0019760 78.5511 281.7832 14.19318836816214
Epoch (UTC): | 09 June 2023 22:11:21 |
Eccentricity: | 0.0019760 |
inclination: | 71.0157° |
perigee height: | 813 km |
apogee height: | 842 km |
right ascension of ascending node: | 30.5070° |
argument of perigee: | 78.5511° |
revolutions per day: | 14.19318836 |
mean anomaly at epoch: | 281.7832° |
orbit number at epoch: | 81621 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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