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 24282.36690998 .00049831 00000-0 51983-2 0 9993
2 39446 97.7918 229.8873 0056831 205.1014 154.7438 14.88339400585521
Epoch (UTC): | 08 October 2024 08:48:21 |
Eccentricity: | 0.0056831 |
inclination: | 97.7918° |
perigee height: | 563 km |
apogee height: | 643 km |
right ascension of ascending node: | 229.8873° |
argument of perigee: | 205.1014° |
revolutions per day: | 14.88339400 |
mean anomaly at epoch: | 154.7438° |
orbit number at epoch: | 58552 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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