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 23086.04715188 .00054095 00000-0 56602-3 0 9994
2 48274 41.4738 296.8673 0003282 238.4397 252.6242 15.63562740108984
Epoch (UTC): | 27 March 2023 01:07:53 |
Eccentricity: | 0.0003282 |
inclination: | 41.4738° |
perigee height: | 375 km |
apogee height: | 379 km |
right ascension of ascending node: | 296.8673° |
argument of perigee: | 238.4397° |
revolutions per day: | 15.63562740 |
mean anomaly at epoch: | 252.6242° |
orbit number at epoch: | 10898 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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