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 22135.89363366 .00000525 00000-0 73387-4 0 9998
2 44881 97.8925 215.5687 0013744 294.8923 65.0848 14.81682261129953
Epoch (UTC): | 15 May 2022 21:26:49 |
Eccentricity: | 0.0013744 |
inclination: | 97.8925° |
perigee height: | 614 km |
apogee height: | 633 km |
right ascension of ascending node: | 215.5687° |
argument of perigee: | 294.8923° |
revolutions per day: | 14.81682261 |
mean anomaly at epoch: | 65.0848° |
orbit number at epoch: | 12995 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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