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 39087U 13009B 24315.79781556 .00003473 00000-0 11498-2 0 9995
2 39087 98.3651 142.5326 0011962 159.1393 201.0285 14.38473810613258
Epoch (UTC): | 10 November 2024 19:08:51 |
Eccentricity: | 0.0011962 |
inclination: | 98.3651° |
perigee height: | 755 km |
apogee height: | 772 km |
right ascension of ascending node: | 142.5326° |
argument of perigee: | 159.1393° |
revolutions per day: | 14.38473810 |
mean anomaly at epoch: | 201.0285° |
orbit number at epoch: | 61325 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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