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 39135U 13015F 23338.47574184 .00356340 00000-0 16500-2 0 9995
2 39135 64.8410 114.6267 0010388 285.6539 74.3472 15.82196874588853
| Epoch (UTC): | 04 December 2023 11:25:04 |
| Eccentricity: | 0.0010388 |
| inclination: | 64.8410° |
| perigee height: | 317 km |
| apogee height: | 331 km |
| right ascension of ascending node: | 114.6267° |
| argument of perigee: | 285.6539° |
| revolutions per day: | 15.82196874 |
| mean anomaly at epoch: | 74.3472° |
| orbit number at epoch: | 58885 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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