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 48274U 21035A 22182.85659337 -.00000612 00000-0 -31731-5 0 9998
2 48274 41.4716 129.7049 0001994 350.3097 39.1050 15.60688530 67061
Epoch (UTC): | 01 July 2022 20:33:29 |
Eccentricity: | 0.0001994 |
inclination: | 41.4716° |
perigee height: | 384 km |
apogee height: | 387 km |
right ascension of ascending node: | 129.7049° |
argument of perigee: | 350.3097° |
revolutions per day: | 15.60688530 |
mean anomaly at epoch: | 39.1050° |
orbit number at epoch: | 6706 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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