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 11289U 79021B 23150.48601478 .00000104 00000-0 48864-4 0 9998
2 11289 81.2471 203.7027 0075590 185.3875 174.6493 14.11731018277197
Epoch (UTC): | 30 May 2023 11:39:51 |
Eccentricity: | 0.0075590 |
inclination: | 81.2471° |
perigee height: | 799 km |
apogee height: | 908 km |
right ascension of ascending node: | 203.7027° |
argument of perigee: | 185.3875° |
revolutions per day: | 14.11731018 |
mean anomaly at epoch: | 174.6493° |
orbit number at epoch: | 27719 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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