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 22829U 93061G 23088.36065238 .00000281 00000-0 12382-3 0 9996
2 22829 98.8290 130.7356 0008923 233.9362 126.0994 14.31249453539819
Epoch (UTC): | 29 March 2023 08:39:20 |
Eccentricity: | 0.0008923 |
inclination: | 98.8290° |
perigee height: | 781 km |
apogee height: | 794 km |
right ascension of ascending node: | 130.7356° |
argument of perigee: | 233.9362° |
revolutions per day: | 14.31249453 |
mean anomaly at epoch: | 126.0994° |
orbit number at epoch: | 53981 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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