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 28222U 04012C 24317.05755547 .00026936 00000-0 83227-3 0 9999
2 28222 97.7961 337.1820 0028083 249.9004 109.9215 15.33113428129718
Epoch (UTC): | 12 November 2024 01:22:52 |
Eccentricity: | 0.0028083 |
inclination: | 97.7961° |
perigee height: | 447 km |
apogee height: | 486 km |
right ascension of ascending node: | 337.1820° |
argument of perigee: | 249.9004° |
revolutions per day: | 15.33113428 |
mean anomaly at epoch: | 109.9215° |
orbit number at epoch: | 12971 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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