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 39446U 13066AG 24262.39524354 .00011738 00000-0 12522-2 0 9997
2 39446 97.7880 210.2621 0056097 273.0466 86.4332 14.87833019582551
Epoch (UTC): | 18 September 2024 09:29:09 |
Eccentricity: | 0.0056097 |
inclination: | 97.7880° |
perigee height: | 565 km |
apogee height: | 644 km |
right ascension of ascending node: | 210.2621° |
argument of perigee: | 273.0466° |
revolutions per day: | 14.87833019 |
mean anomaly at epoch: | 86.4332° |
orbit number at epoch: | 58255 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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