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 12744U 81053CM 23027.46780384 .00003844 00000-0 18660-2 0 9991
2 12744 82.9351 17.7600 0021569 266.5166 93.3547 14.18001961113999
Epoch (UTC): | 27 January 2023 11:13:38 |
Eccentricity: | 0.0021569 |
inclination: | 82.9351° |
perigee height: | 816 km |
apogee height: | 847 km |
right ascension of ascending node: | 17.7600° |
argument of perigee: | 266.5166° |
revolutions per day: | 14.18001961 |
mean anomaly at epoch: | 93.3547° |
orbit number at epoch: | 11399 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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