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 23265.43379096 .00021440 00000-0 23484-3 0 9990
2 48274 41.4738 284.2441 0007949 81.1917 278.9822 15.62720380137031
Epoch (UTC): | 22 September 2023 10:24:39 |
Eccentricity: | 0.0007949 |
inclination: | 41.4738° |
perigee height: | 374 km |
apogee height: | 385 km |
right ascension of ascending node: | 284.2441° |
argument of perigee: | 81.1917° |
revolutions per day: | 15.62720380 |
mean anomaly at epoch: | 278.9822° |
orbit number at epoch: | 13703 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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