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 27875U 03040A 23081.32135486 -.00000285 00000-0 00000+0 0 9997
2 27875 7.9705 57.9386 0002367 332.2703 222.5422 1.00267200 19765
Epoch (UTC): | 22 March 2023 07:42:45 |
Eccentricity: | 0.0002367 |
inclination: | 7.9705° |
perigee height: | 35777 km |
apogee height: | 35797 km |
right ascension of ascending node: | 57.9386° |
argument of perigee: | 332.2703° |
revolutions per day: | 1.00267200 |
mean anomaly at epoch: | 222.5422° |
orbit number at epoch: | 1976 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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