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 18422U 87088B 23151.86753983 .00000536 00000-0 61861-4 0 9999
2 18422 82.5102 298.6077 0020780 113.2476 247.0930 14.83579781924134
Epoch (UTC): | 31 May 2023 20:49:15 |
Eccentricity: | 0.0020780 |
inclination: | 82.5102° |
perigee height: | 603 km |
apogee height: | 632 km |
right ascension of ascending node: | 298.6077° |
argument of perigee: | 113.2476° |
revolutions per day: | 14.83579781 |
mean anomaly at epoch: | 247.0930° |
orbit number at epoch: | 92413 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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