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 25992U 99067B 24358.03919635 .00007351 00000-0 21730-2 0 9997
2 25992 98.2119 17.0083 0006224 161.0262 226.3789 14.43723196305689
Epoch (UTC): | 23 December 2024 00:56:26 |
Eccentricity: | 0.0006224 |
inclination: | 98.2119° |
perigee height: | 742 km |
apogee height: | 750 km |
right ascension of ascending node: | 17.0083° |
argument of perigee: | 161.0262° |
revolutions per day: | 14.43723196 |
mean anomaly at epoch: | 226.3789° |
orbit number at epoch: | 30568 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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