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 44711U 19039N 23336.38768566 .00323205 00000-0 64700-1 0 9998
2 44711 97.3030 132.1200 0261454 235.5273 122.0971 14.40820477213453
Epoch (UTC): | 02 December 2023 09:18:16 |
Eccentricity: | 0.0261454 |
inclination: | 97.3030° |
perigee height: | 569 km |
apogee height: | 942 km |
right ascension of ascending node: | 132.1200° |
argument of perigee: | 235.5273° |
revolutions per day: | 14.40820477 |
mean anomaly at epoch: | 122.0971° |
orbit number at epoch: | 21345 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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