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 22139.13411012 -.00000011 00000-0 45889-4 0 9992
2 36095 67.1477 275.8786 0006318 243.4426 116.6011 13.96790138637204
Epoch (UTC): | 19 May 2022 03:13:07 |
Eccentricity: | 0.0006318 |
inclination: | 67.1477° |
perigee height: | 900 km |
apogee height: | 909 km |
right ascension of ascending node: | 275.8786° |
argument of perigee: | 243.4426° |
revolutions per day: | 13.96790138 |
mean anomaly at epoch: | 116.6011° |
orbit number at epoch: | 63720 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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