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 39430U 13066Q 23340.14702893 .00002022 00000-0 34930-3 0 9999
2 39430 97.7562 221.1439 0143681 148.3140 212.6812 14.62849625534666
Epoch (UTC): | 06 December 2023 03:31:43 |
Eccentricity: | 0.0143681 |
inclination: | 97.7562° |
perigee height: | 582 km |
apogee height: | 785 km |
right ascension of ascending node: | 221.1439° |
argument of perigee: | 148.3140° |
revolutions per day: | 14.62849625 |
mean anomaly at epoch: | 212.6812° |
orbit number at epoch: | 53466 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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