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 39136U 13015G 24031.81149100 .08315843 75848-5 10855-2 0 9996
2 39136 64.8280 284.0616 0007840 244.6079 115.4293 16.35178941597292
| Epoch (UTC): | 31 January 2024 19:28:32 |
| Eccentricity: | 0.0007840 |
| inclination: | 64.8280° |
| perigee height: | 173 km |
| apogee height: | 184 km |
| right ascension of ascending node: | 284.0616° |
| argument of perigee: | 244.6079° |
| revolutions per day: | 16.35178941 |
| mean anomaly at epoch: | 115.4293° |
| orbit number at epoch: | 59729 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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