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 23091.21460968 .00001855 00000-0 23827-3 0 9992
2 44881 97.8641 170.9763 0014287 334.3082 25.7422 14.82329162177397
Epoch (UTC): | 01 April 2023 05:09:02 |
Eccentricity: | 0.0014287 |
inclination: | 97.8641° |
perigee height: | 612 km |
apogee height: | 632 km |
right ascension of ascending node: | 170.9763° |
argument of perigee: | 334.3082° |
revolutions per day: | 14.82329162 |
mean anomaly at epoch: | 25.7422° |
orbit number at epoch: | 17739 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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