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 22138.45984322 .00000689 00000-0 94176-4 0 9994
2 44881 97.8928 218.0985 0013693 285.5716 74.3992 14.81687363130330
Epoch (UTC): | 18 May 2022 11:02:10 |
Eccentricity: | 0.0013693 |
inclination: | 97.8928° |
perigee height: | 614 km |
apogee height: | 633 km |
right ascension of ascending node: | 218.0985° |
argument of perigee: | 285.5716° |
revolutions per day: | 14.81687363 |
mean anomaly at epoch: | 74.3992° |
orbit number at epoch: | 13033 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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