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 23342.48735133 .00123117 00000-0 10961-2 0 9994
2 39136 64.8560 117.6968 0017667 268.0035 91.9092 15.67669439588694
| Epoch (UTC): | 08 December 2023 11:41:47 |
| Eccentricity: | 0.0017667 |
| inclination: | 64.8560° |
| perigee height: | 353 km |
| apogee height: | 377 km |
| right ascension of ascending node: | 117.6968° |
| argument of perigee: | 268.0035° |
| revolutions per day: | 15.67669439 |
| mean anomaly at epoch: | 91.9092° |
| orbit number at epoch: | 58869 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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