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 14781U 84021B 22184.90696872 .00000330 00000-0 45994-4 0 9991
2 14781 97.6176 171.5914 0006789 267.7416 92.3022 14.83698196 42481
Epoch (UTC): | 03 July 2022 21:46:02 |
Eccentricity: | 0.0006789 |
inclination: | 97.6176° |
perigee height: | 613 km |
apogee height: | 622 km |
right ascension of ascending node: | 171.5914° |
argument of perigee: | 267.7416° |
revolutions per day: | 14.83698196 |
mean anomaly at epoch: | 92.3022° |
orbit number at epoch: | 4248 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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