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 39105U 86019VT 24251.33203386 .00002284 00000-0 12162-2 0 9994
2 39105 98.6005 281.2177 0116087 333.3338 26.1893 14.10958788101591
| Epoch (UTC): | 07 September 2024 07:58:07 |
| Eccentricity: | 0.0116087 |
| inclination: | 98.6005° |
| perigee height: | 772 km |
| apogee height: | 940 km |
| right ascension of ascending node: | 281.2177° |
| argument of perigee: | 333.3338° |
| revolutions per day: | 14.10958788 |
| mean anomaly at epoch: | 26.1893° |
| orbit number at epoch: | 10159 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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