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 37855U 11061F 22181.27149922 .00003396 00000-0 15344-3 0 9998
2 37855 101.7115 307.1296 0152534 23.9731 336.8490 15.12591935583177
Epoch (UTC): | 30 June 2022 06:30:57 |
Eccentricity: | 0.0152534 |
inclination: | 101.7115° |
perigee height: | 423 km |
apogee height: | 633 km |
right ascension of ascending node: | 307.1296° |
argument of perigee: | 23.9731° |
revolutions per day: | 15.12591935 |
mean anomaly at epoch: | 336.8490° |
orbit number at epoch: | 58317 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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