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 59U 60013B 24311.15752041 .00000275 00000-0 25181-3 0 9994
2 59 28.2479 264.9483 0189047 59.0295 302.8681 13.53107335164339
Epoch (UTC): | 06 November 2024 03:46:49 |
Eccentricity: | 0.0189047 |
inclination: | 28.2479° |
perigee height: | 920 km |
apogee height: | 1201 km |
right ascension of ascending node: | 264.9483° |
argument of perigee: | 59.0295° |
revolutions per day: | 13.53107335 |
mean anomaly at epoch: | 302.8681° |
orbit number at epoch: | 16433 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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