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 is defined by the following mean orbital elements,
1 39650U 14019A 24091.02195825 0.00100000 00000-0 18966-2 0 02
2 39650 140.7411 220.1855 0001000 234.6001 125.3991 15.47379693 07
| Epoch (UTC): | 31 March 2024 00:31:37 |
| Eccentricity: | 0.0001000 |
| inclination: | 140.7411° |
| perigee height: | 424 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 220.1855° |
| argument of perigee: | 234.6001° |
| revolutions per day: | 15.47379693 |
| mean anomaly at epoch: | 125.3991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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