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 00022U 59009A 24311.84376158 .00022549 00000-0 11456-2 0 9991
2 00022 50.2761 88.6229 0104820 305.8178 53.3071 15.12035107710955
Epoch (UTC): | 06 November 2024 20:15:01 |
Eccentricity: | 0.0104820 |
inclination: | 50.2761° |
perigee height: | 457 km |
apogee height: | 602 km |
right ascension of ascending node: | 88.6229° |
argument of perigee: | 305.8178° |
revolutions per day: | 15.12035107 |
mean anomaly at epoch: | 53.3071° |
orbit number at epoch: | 71095 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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