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 23089.46124016 .00003507 00000-0 61835-3 0 9992
2 39430 97.7880 345.1764 0145276 222.0753 136.9137 14.61430434498041
Epoch (UTC): | 30 March 2023 11:04:11 |
Eccentricity: | 0.0145276 |
inclination: | 97.7880° |
perigee height: | 586 km |
apogee height: | 791 km |
right ascension of ascending node: | 345.1764° |
argument of perigee: | 222.0753° |
revolutions per day: | 14.61430434 |
mean anomaly at epoch: | 136.9137° |
orbit number at epoch: | 49804 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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