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 21820U 91086B 25193.79682417 .00000301 00000-0 59418-4 0 9996
2 21820 82.5609 177.7155 1562511 230.3601 114.9079 11.96273273458564
Epoch (UTC): | 12 July 2025 19:07:25 |
Eccentricity: | 0.1562511 |
inclination: | 82.5609° |
perigee height: | 436 km |
apogee height: | 2959 km |
right ascension of ascending node: | 177.7155° |
argument of perigee: | 230.3601° |
revolutions per day: | 11.96273273 |
mean anomaly at epoch: | 114.9079° |
orbit number at epoch: | 45856 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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