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 5U 58002B 22186.06926835 .00000254 00000-0 33556-3 0 9994
2 5 34.2470 85.1281 1847114 116.8265 263.2842 10.84970452286550
Epoch (UTC): | 05 July 2022 01:39:44 |
Eccentricity: | 0.1847114 |
inclination: | 34.2470° |
perigee height: | 649 km |
apogee height: | 3833 km |
right ascension of ascending node: | 85.1281° |
argument of perigee: | 116.8265° |
revolutions per day: | 10.84970452 |
mean anomaly at epoch: | 263.2842° |
orbit number at epoch: | 28655 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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