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 37348U 11002A 22221.99742264 0.00038669 00000-0 23180-3 0 03
2 37348 98.0456 354.1220 0382559 178.8340 181.3367 15.18127660 05
Epoch (UTC): | 09 August 2022 23:56:17 |
Eccentricity: | 0.0382559 |
inclination: | 98.0456° |
perigee height: | 248 km |
apogee height: | 775 km |
right ascension of ascending node: | 354.1220° |
argument of perigee: | 178.8340° |
revolutions per day: | 15.18127660 |
mean anomaly at epoch: | 181.3367° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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