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 27141U 01049CM 24281.50406420 .00008296 00000-0 90692-3 0 9991
2 27141 98.1585 307.5166 0050637 96.4487 40.6856 14.87175313230172
Epoch (UTC): | 07 October 2024 12:05:51 |
Eccentricity: | 0.0050637 |
inclination: | 98.1585° |
perigee height: | 571 km |
apogee height: | 642 km |
right ascension of ascending node: | 307.5166° |
argument of perigee: | 96.4487° |
revolutions per day: | 14.87175313 |
mean anomaly at epoch: | 40.6856° |
orbit number at epoch: | 23017 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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