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 08027U 75064B 22222.58852843 -.00000019 00000-0 -18530-4 0 9995
2 08027 81.2937 44.4592 0056978 3.2816 356.8716 14.07389151416693
Epoch (UTC): | 10 August 2022 14:07:28 |
Eccentricity: | 0.0056978 |
inclination: | 81.2937° |
perigee height: | 827 km |
apogee height: | 909 km |
right ascension of ascending node: | 44.4592° |
argument of perigee: | 3.2816° |
revolutions per day: | 14.07389151 |
mean anomaly at epoch: | 356.8716° |
orbit number at epoch: | 41669 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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