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 44881U 19093C 23335.85714415 .00002525 00000-0 31650-3 0 9990
2 44881 97.8488 51.3848 0013284 249.2048 110.7743 14.83040836213643
Epoch (UTC): | 01 December 2023 20:34:17 |
Eccentricity: | 0.0013284 |
inclination: | 97.8488° |
perigee height: | 610 km |
apogee height: | 629 km |
right ascension of ascending node: | 51.3848° |
argument of perigee: | 249.2048° |
revolutions per day: | 14.83040836 |
mean anomaly at epoch: | 110.7743° |
orbit number at epoch: | 21364 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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