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 23159.14181961 -.00000012 00000-0 45153-4 0 9998
2 36095 67.1490 59.9233 0008791 257.8415 102.1685 13.96839986690785
Epoch (UTC): | 08 June 2023 03:24:13 |
Eccentricity: | 0.0008791 |
inclination: | 67.1490° |
perigee height: | 898 km |
apogee height: | 911 km |
right ascension of ascending node: | 59.9233° |
argument of perigee: | 257.8415° |
revolutions per day: | 13.96839986 |
mean anomaly at epoch: | 102.1685° |
orbit number at epoch: | 69078 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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