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 21015U 90111B 25135.66213854 .00000253 00000-0 93734-4 0 9992
2 21015 74.0505 235.6925 0020890 147.2157 213.0297 14.37073885900920
Epoch (UTC): | 15 May 2025 15:53:28 |
Eccentricity: | 0.0020890 |
inclination: | 74.0505° |
perigee height: | 753 km |
apogee height: | 783 km |
right ascension of ascending node: | 235.6925° |
argument of perigee: | 147.2157° |
revolutions per day: | 14.37073885 |
mean anomaly at epoch: | 213.0297° |
orbit number at epoch: | 90092 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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