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 23156.49257524 -.00000029 00000-0 33602-4 0 9996
2 36095 67.1488 66.3637 0008810 258.4079 101.6016 13.96839784690606
Epoch (UTC): | 05 June 2023 11:49:18 |
Eccentricity: | 0.0008810 |
inclination: | 67.1488° |
perigee height: | 898 km |
apogee height: | 911 km |
right ascension of ascending node: | 66.3637° |
argument of perigee: | 258.4079° |
revolutions per day: | 13.96839784 |
mean anomaly at epoch: | 101.6016° |
orbit number at epoch: | 69060 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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