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 25544U 98067A 25140.37106448 .00008533 00000-0 15939-3 0 9994
2 25544 51.6374 84.8753 0002567 126.2244 18.1297 15.49625942510847
Epoch (UTC): | 20 May 2025 08:54:19 |
Eccentricity: | 0.0002567 |
inclination: | 51.6374° |
perigee height: | 416 km |
apogee height: | 419 km |
right ascension of ascending node: | 84.8753° |
argument of perigee: | 126.2244° |
revolutions per day: | 15.49625942 |
mean anomaly at epoch: | 18.1297° |
orbit number at epoch: | 51084 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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