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 27711U 03012A 23341.50994427 -.00000176 00000-0 00000-0 0 9992
2 27711 10.9354 36.7090 0096788 356.2354 18.8098 1.00273612 23701
Epoch (UTC): | 07 December 2023 12:14:19 |
Eccentricity: | 0.0096788 |
inclination: | 10.9354° |
perigee height: | 35377 km |
apogee height: | 36194 km |
right ascension of ascending node: | 36.7090° |
argument of perigee: | 356.2354° |
revolutions per day: | 1.00273612 |
mean anomaly at epoch: | 18.8098° |
orbit number at epoch: | 2370 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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