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 27386U 02009A 24309.86115060 .00000851 00000-0 29097-3 0 9996
2 27386 98.3026 266.1979 0001333 83.9725 330.0456 14.38744511188804
Epoch (UTC): | 04 November 2024 20:40:03 |
Eccentricity: | 0.0001333 |
inclination: | 98.3026° |
perigee height: | 762 km |
apogee height: | 763 km |
right ascension of ascending node: | 266.1979° |
argument of perigee: | 83.9725° |
revolutions per day: | 14.38744511 |
mean anomaly at epoch: | 330.0456° |
orbit number at epoch: | 18880 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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