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 00053U 60009E 24312.55358303 -.00000054 00000-0 30702-3 0 9992
2 00053 47.2789 351.8671 0098550 143.0828 217.6795 12.17354972863961
Epoch (UTC): | 07 November 2024 13:17:09 |
Eccentricity: | 0.0098550 |
inclination: | 47.2789° |
perigee height: | 1525 km |
apogee height: | 1683 km |
right ascension of ascending node: | 351.8671° |
argument of perigee: | 143.0828° |
revolutions per day: | 12.17354972 |
mean anomaly at epoch: | 217.6795° |
orbit number at epoch: | 86396 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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