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 24262.79876279 .00008245 00000-0 88178-3 0 9997
2 39446 97.7883 210.6584 0056019 271.6768 87.8032 14.87837088582618
Epoch (UTC): | 18 September 2024 19:10:13 |
Eccentricity: | 0.0056019 |
inclination: | 97.7883° |
perigee height: | 565 km |
apogee height: | 644 km |
right ascension of ascending node: | 210.6584° |
argument of perigee: | 271.6768° |
revolutions per day: | 14.87837088 |
mean anomaly at epoch: | 87.8032° |
orbit number at epoch: | 58261 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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