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 23335.97448209 .00004480 00000-0 76440-3 0 9994
2 39430 97.7560 217.2193 0143418 161.5026 199.1469 14.62827158534052
Epoch (UTC): | 01 December 2023 23:23:15 |
Eccentricity: | 0.0143418 |
inclination: | 97.7560° |
perigee height: | 583 km |
apogee height: | 785 km |
right ascension of ascending node: | 217.2193° |
argument of perigee: | 161.5026° |
revolutions per day: | 14.62827158 |
mean anomaly at epoch: | 199.1469° |
orbit number at epoch: | 53405 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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