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 22148.54841288 .00024401 00000-0 29311-3 0 9993
2 48274 41.4724 338.3139 0001353 85.3138 307.2767 15.60302398 61702
Epoch (UTC): | 28 May 2022 13:09:42 |
Eccentricity: | 0.0001353 |
inclination: | 41.4724° |
perigee height: | 386 km |
apogee height: | 388 km |
right ascension of ascending node: | 338.3139° |
argument of perigee: | 85.3138° |
revolutions per day: | 15.60302398 |
mean anomaly at epoch: | 307.2767° |
orbit number at epoch: | 6170 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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