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 23276.87027269 .00051022 00000-0 53275-3 0 9992
2 48274 41.4730 214.4058 0009718 180.8345 179.2480 15.63585104138825
Epoch (UTC): | 03 October 2023 20:53:11 |
Eccentricity: | 0.0009718 |
inclination: | 41.4730° |
perigee height: | 371 km |
apogee height: | 384 km |
right ascension of ascending node: | 214.4058° |
argument of perigee: | 180.8345° |
revolutions per day: | 15.63585104 |
mean anomaly at epoch: | 179.2480° |
orbit number at epoch: | 13882 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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