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 39652U 14020A 22263.91318420 0.00000000 00000-0 00000-0 0 08
2 39652 2.2006 50.4699 0007516 86.9098 273.1965 1.00270000 02
| Epoch (UTC): | 20 September 2022 21:54:59 |
| Eccentricity: | 0.0007516 |
| inclination: | 2.2006° |
| perigee height: | 35755 km |
| apogee height: | 35818 km |
| right ascension of ascending node: | 50.4699° |
| argument of perigee: | 86.9098° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 273.1965° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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