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 39440U 13066AA 23091.11851463 .00006426 00000-0 83973-3 0 9991
2 39440 97.7644 42.4531 0074347 278.2288 81.0496 14.78860633503967
| Epoch (UTC): | 01 April 2023 02:50:39 |
| Eccentricity: | 0.0074347 |
| inclination: | 97.7644° |
| perigee height: | 581 km |
| apogee height: | 685 km |
| right ascension of ascending node: | 42.4531° |
| argument of perigee: | 278.2288° |
| revolutions per day: | 14.78860633 |
| mean anomaly at epoch: | 81.0496° |
| orbit number at epoch: | 50396 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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