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 39107U 86019VV 24356.86712605 .00001840 00000-0 96180-3 0 9999
2 39107 98.7023 28.1827 0152794 106.8748 254.9241 14.09720334588271
| Epoch (UTC): | 21 December 2024 20:48:39 |
| Eccentricity: | 0.0152794 |
| inclination: | 98.7023° |
| perigee height: | 750 km |
| apogee height: | 971 km |
| right ascension of ascending node: | 28.1827° |
| argument of perigee: | 106.8748° |
| revolutions per day: | 14.09720334 |
| mean anomaly at epoch: | 254.9241° |
| orbit number at epoch: | 58827 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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