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 00045U 60007A 24311.80431785 .00002475 00000-0 62104-3 0 9993
2 00045 66.6936 112.9772 0256964 228.9306 128.9343 14.35089411295730
Epoch (UTC): | 06 November 2024 19:18:13 |
Eccentricity: | 0.0256964 |
inclination: | 66.6936° |
perigee height: | 591 km |
apogee height: | 958 km |
right ascension of ascending node: | 112.9772° |
argument of perigee: | 228.9306° |
revolutions per day: | 14.35089411 |
mean anomaly at epoch: | 128.9343° |
orbit number at epoch: | 29573 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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