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 23087.70446230 .00002131 00000-0 27272-3 0 9993
2 44881 97.8646 167.5253 0014515 346.0844 13.9976 14.82317294176876
Epoch (UTC): | 28 March 2023 16:54:25 |
Eccentricity: | 0.0014515 |
inclination: | 97.8646° |
perigee height: | 612 km |
apogee height: | 632 km |
right ascension of ascending node: | 167.5253° |
argument of perigee: | 346.0844° |
revolutions per day: | 14.82317294 |
mean anomaly at epoch: | 13.9976° |
orbit number at epoch: | 17687 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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