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 39136U 13015G 23087.54289415 .00040968 00000-0 12229-2 0 9995
2 39136 64.8701 256.7556 0025976 280.0963 79.7241 15.34068385549284
Epoch (UTC): | 28 March 2023 13:01:46 |
Eccentricity: | 0.0025976 |
inclination: | 64.8701° |
perigee height: | 446 km |
apogee height: | 481 km |
right ascension of ascending node: | 256.7556° |
argument of perigee: | 280.0963° |
revolutions per day: | 15.34068385 |
mean anomaly at epoch: | 79.7241° |
orbit number at epoch: | 54928 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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