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 24280.82053570 .00014744 00000-0 15537-2 0 9991
2 39446 97.7924 228.3661 0056660 210.2503 149.5440 14.88243214585293
Epoch (UTC): | 06 October 2024 19:41:34 |
Eccentricity: | 0.0056660 |
inclination: | 97.7924° |
perigee height: | 564 km |
apogee height: | 643 km |
right ascension of ascending node: | 228.3661° |
argument of perigee: | 210.2503° |
revolutions per day: | 14.88243214 |
mean anomaly at epoch: | 149.5440° |
orbit number at epoch: | 58529 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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