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 24311.89531102 .00000282 00000-0 26140-3 0 9992
2 00059 28.2478 261.1575 0189049 65.2214 296.7875 13.53107698163563
Epoch (UTC): | 06 November 2024 21:29:14 |
Eccentricity: | 0.0189049 |
inclination: | 28.2478° |
perigee height: | 920 km |
apogee height: | 1201 km |
right ascension of ascending node: | 261.1575° |
argument of perigee: | 65.2214° |
revolutions per day: | 13.53107698 |
mean anomaly at epoch: | 296.7875° |
orbit number at epoch: | 16356 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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