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 41310U 16005A 25114.17576971 .00000064 00000-0 00000+0 0 9996
2 41310 0.0709 71.4317 0003387 287.9799 285.3144 1.00271604 33905
Epoch (UTC): | 24 April 2025 04:13:06 |
Eccentricity: | 0.0003387 |
inclination: | 0.0709° |
perigee height: | 35772 km |
apogee height: | 35800 km |
right ascension of ascending node: | 71.4317° |
argument of perigee: | 287.9799° |
revolutions per day: | 1.00271604 |
mean anomaly at epoch: | 285.3144° |
orbit number at epoch: | 3390 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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