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 22803U 93059B 23159.50978420 .00000287 00000-0 16673-3 0 9999
2 22803 70.9902 330.3601 0019059 298.3624 61.5577 14.16936759537139
Epoch (UTC): | 08 June 2023 12:14:05 |
Eccentricity: | 0.0019059 |
inclination: | 70.9902° |
perigee height: | 822 km |
apogee height: | 849 km |
right ascension of ascending node: | 330.3601° |
argument of perigee: | 298.3624° |
revolutions per day: | 14.16936759 |
mean anomaly at epoch: | 61.5577° |
orbit number at epoch: | 53713 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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