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 10143U 77065A 23087.52241608 -.00000270 00000-0 00000-0 0 9992
2 10143 9.3205 303.5556 0017557 202.9619 349.6393 0.99250482109546
Epoch (UTC): | 28 March 2023 12:32:16 |
Eccentricity: | 0.0017557 |
inclination: | 9.3205° |
perigee height: | 36000 km |
apogee height: | 36149 km |
right ascension of ascending node: | 303.5556° |
argument of perigee: | 202.9619° |
revolutions per day: | 0.99250482 |
mean anomaly at epoch: | 349.6393° |
orbit number at epoch: | 10954 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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