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 54910U 22151QX 24251.59788333 .00557292 00000-0 31799-1 0 9990
2 54910 98.8010 305.9138 0056380 102.4873 258.2667 15.09195373 20688
Epoch (UTC): | 07 September 2024 14:20:57 |
Eccentricity: | 0.0056380 |
inclination: | 98.8010° |
perigee height: | 499 km |
apogee height: | 577 km |
right ascension of ascending node: | 305.9138° |
argument of perigee: | 102.4873° |
revolutions per day: | 15.09195373 |
mean anomaly at epoch: | 258.2667° |
orbit number at epoch: | 2068 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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