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 27609U 02058E 23334.42310328 .00001225 00000-0 18206-3 0 9997
2 27609 64.5563 321.4109 0013977 188.1127 171.9753 14.79467050130213
Epoch (UTC): | 30 November 2023 10:09:16 |
Eccentricity: | 0.0013977 |
inclination: | 64.5563° |
perigee height: | 621 km |
apogee height: | 641 km |
right ascension of ascending node: | 321.4109° |
argument of perigee: | 188.1127° |
revolutions per day: | 14.79467050 |
mean anomaly at epoch: | 171.9753° |
orbit number at epoch: | 13021 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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