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 23154.45808047 .00000307 00000-0 18368-3 0 9998
2 19649 70.9983 175.6656 0007401 250.6991 109.3331 14.14838636782233
Epoch (UTC): | 03 June 2023 10:59:38 |
Eccentricity: | 0.0007401 |
inclination: | 70.9983° |
perigee height: | 837 km |
apogee height: | 848 km |
right ascension of ascending node: | 175.6656° |
argument of perigee: | 250.6991° |
revolutions per day: | 14.14838636 |
mean anomaly at epoch: | 109.3331° |
orbit number at epoch: | 78223 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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