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 23273.16525442 .00023465 00000-0 25151-3 0 9999
2 48274 41.4731 237.0400 0008759 151.7194 208.4123 15.63223751138243
Epoch (UTC): | 30 September 2023 03:57:57 |
Eccentricity: | 0.0008759 |
inclination: | 41.4731° |
perigee height: | 372 km |
apogee height: | 384 km |
right ascension of ascending node: | 237.0400° |
argument of perigee: | 151.7194° |
revolutions per day: | 15.63223751 |
mean anomaly at epoch: | 208.4123° |
orbit number at epoch: | 13824 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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