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 23160.54674791 .00020616 00000-0 25187-3 0 9992
2 48274 41.4734 202.3095 0002979 320.8913 39.1710 15.59933405120642
Epoch (UTC): | 09 June 2023 13:07:19 |
Eccentricity: | 0.0002979 |
inclination: | 41.4734° |
perigee height: | 386 km |
apogee height: | 390 km |
right ascension of ascending node: | 202.3095° |
argument of perigee: | 320.8913° |
revolutions per day: | 15.59933405 |
mean anomaly at epoch: | 39.1710° |
orbit number at epoch: | 12064 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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