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 14780U 84021A 25199.77871527 .00001222 00000-0 92678-4 0 9998
2 14780 98.0841 99.7580 0073420 151.9473 208.5738 15.02213523741296
Epoch (UTC): | 18 July 2025 18:41:20 |
Eccentricity: | 0.0073420 |
inclination: | 98.0841° |
perigee height: | 509 km |
apogee height: | 611 km |
right ascension of ascending node: | 99.7580° |
argument of perigee: | 151.9473° |
revolutions per day: | 15.02213523 |
mean anomaly at epoch: | 208.5738° |
orbit number at epoch: | 74129 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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