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 35935U 09051E 24262.17550454 .00003176 00000-0 69778-3 0 9994
2 35935 98.4582 147.8281 0009135 56.5667 303.6404 14.58228567795848
Epoch (UTC): | 18 September 2024 04:12:43 |
Eccentricity: | 0.0009135 |
inclination: | 98.4582° |
perigee height: | 692 km |
apogee height: | 705 km |
right ascension of ascending node: | 147.8281° |
argument of perigee: | 56.5667° |
revolutions per day: | 14.58228567 |
mean anomaly at epoch: | 303.6404° |
orbit number at epoch: | 79584 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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