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 19649U 88102A 22230.00241970 .00000322 00000-0 19162-3 0 9999
2 19649 70.9999 63.3126 0006781 311.0177 49.0358 14.14771744741569
Epoch (UTC): | 18 August 2022 00:03:29 |
Eccentricity: | 0.0006781 |
inclination: | 70.9999° |
perigee height: | 838 km |
apogee height: | 848 km |
right ascension of ascending node: | 63.3126° |
argument of perigee: | 311.0177° |
revolutions per day: | 14.14771744 |
mean anomaly at epoch: | 49.0358° |
orbit number at epoch: | 74156 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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