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 36095U 09063A 23151.91009748 .00000078 00000-0 10978-3 0 9994
2 36095 67.1485 77.5041 0008913 259.5578 100.4503 13.96839585689779
Epoch (UTC): | 31 May 2023 21:50:32 |
Eccentricity: | 0.0008913 |
inclination: | 67.1485° |
perigee height: | 898 km |
apogee height: | 911 km |
right ascension of ascending node: | 77.5041° |
argument of perigee: | 259.5578° |
revolutions per day: | 13.96839585 |
mean anomaly at epoch: | 100.4503° |
orbit number at epoch: | 68977 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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