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 11870U 80056B 23150.47780116 .00000131 00000-0 52498-4 0 9998
2 11870 74.0515 175.7146 0017403 305.4286 54.5242 14.37330769223120
Epoch (UTC): | 30 May 2023 11:28:02 |
Eccentricity: | 0.0017403 |
inclination: | 74.0515° |
perigee height: | 755 km |
apogee height: | 780 km |
right ascension of ascending node: | 175.7146° |
argument of perigee: | 305.4286° |
revolutions per day: | 14.37330769 |
mean anomaly at epoch: | 54.5242° |
orbit number at epoch: | 22312 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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