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 00059U 60013B 24317.94500306 .00000200 00000-0 14950-3 0 9992
2 00059 28.2470 230.0732 0189078 115.9926 246.0222 13.53109434164385
Epoch (UTC): | 12 November 2024 22:40:48 |
Eccentricity: | 0.0189078 |
inclination: | 28.2470° |
perigee height: | 920 km |
apogee height: | 1201 km |
right ascension of ascending node: | 230.0732° |
argument of perigee: | 115.9926° |
revolutions per day: | 13.53109434 |
mean anomaly at epoch: | 246.0222° |
orbit number at epoch: | 16438 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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