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 24340.99323416 .00018216 00000-0 32316-3 0 9996
2 25544 51.6388 184.2057 0007028 306.7642 201.1123 15.50265976485198
Epoch (UTC): | 05 December 2024 23:50:15 |
Eccentricity: | 0.0007028 |
inclination: | 51.6388° |
perigee height: | 411 km |
apogee height: | 421 km |
right ascension of ascending node: | 184.2057° |
argument of perigee: | 306.7642° |
revolutions per day: | 15.50265976 |
mean anomaly at epoch: | 201.1123° |
orbit number at epoch: | 48519 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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