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 19770U 89005B 22228.30730359 .00000181 00000-0 67117-4 0 9998
2 19770 74.0456 172.6984 0004354 159.5102 312.1122 14.38973110757556
Epoch (UTC): | 16 August 2022 07:22:31 |
Eccentricity: | 0.0004354 |
inclination: | 74.0456° |
perigee height: | 759 km |
apogee height: | 765 km |
right ascension of ascending node: | 172.6984° |
argument of perigee: | 159.5102° |
revolutions per day: | 14.38973110 |
mean anomaly at epoch: | 312.1122° |
orbit number at epoch: | 75755 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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