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 22179.16278018 .00001217 00000-0 16260-3 0 9995
2 39446 97.6860 142.7630 0070085 55.1532 305.6244 14.79595399462634
Epoch (UTC): | 28 June 2022 03:54:24 |
Eccentricity: | 0.0070085 |
inclination: | 97.6860° |
perigee height: | 581 km |
apogee height: | 680 km |
right ascension of ascending node: | 142.7630° |
argument of perigee: | 55.1532° |
revolutions per day: | 14.79595399 |
mean anomaly at epoch: | 305.6244° |
orbit number at epoch: | 46263 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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