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 39485U 13076C 23274.18781535 .00000015 00000-0 36795-4 0 9992
2 39485 82.4803 65.2257 0021876 108.6360 251.7097 12.42878843443112
| Epoch (UTC): | 01 October 2023 04:30:27 |
| Eccentricity: | 0.0021876 |
| inclination: | 82.4803° |
| perigee height: | 1477 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 65.2257° |
| argument of perigee: | 108.6360° |
| revolutions per day: | 12.42878843 |
| mean anomaly at epoch: | 251.7097° |
| orbit number at epoch: | 44311 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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