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 39134U 13015E 23244.86715325 .14409807 78060-5 40554-3 0 9992
2 39134 64.8204 13.5308 0014840 284.7733 75.1809 16.43982745575092
| Epoch (UTC): | 01 September 2023 20:48:42 |
| Eccentricity: | 0.0014840 |
| inclination: | 64.8204° |
| perigee height: | 145 km |
| apogee height: | 165 km |
| right ascension of ascending node: | 13.5308° |
| argument of perigee: | 284.7733° |
| revolutions per day: | 16.43982745 |
| mean anomaly at epoch: | 75.1809° |
| orbit number at epoch: | 57509 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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