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 23275.84828861 .00052265 00000-0 54787-3 0 9994
2 48274 41.4733 220.6499 0009417 173.1842 186.9127 15.63481251138662
Epoch (UTC): | 02 October 2023 20:21:32 |
Eccentricity: | 0.0009417 |
inclination: | 41.4733° |
perigee height: | 371 km |
apogee height: | 384 km |
right ascension of ascending node: | 220.6499° |
argument of perigee: | 173.1842° |
revolutions per day: | 15.63481251 |
mean anomaly at epoch: | 186.9127° |
orbit number at epoch: | 13866 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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