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 39446U 13066AG 23158.77581095 .00004181 00000-0 51388-3 0 9995
2 39446 97.7346 114.0044 0065952 11.4191 348.8500 14.82010269513620
Epoch (UTC): | 07 June 2023 18:37:10 |
Eccentricity: | 0.0065952 |
inclination: | 97.7346° |
perigee height: | 577 km |
apogee height: | 669 km |
right ascension of ascending node: | 114.0044° |
argument of perigee: | 11.4191° |
revolutions per day: | 14.82010269 |
mean anomaly at epoch: | 348.8500° |
orbit number at epoch: | 51362 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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