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 39440U 13066AA 22135.86858877 .00001749 00000-0 24397-3 0 9995
2 39440 97.7240 94.8037 0077430 236.6513 122.7270 14.76907031455473
Epoch (UTC): | 15 May 2022 20:50:46 |
Eccentricity: | 0.0077430 |
inclination: | 97.7240° |
perigee height: | 585 km |
apogee height: | 693 km |
right ascension of ascending node: | 94.8037° |
argument of perigee: | 236.6513° |
revolutions per day: | 14.76907031 |
mean anomaly at epoch: | 122.7270° |
orbit number at epoch: | 45547 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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