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 14781U 84021B 22181.87213727 .00000320 00000-0 44799-4 0 9999
2 14781 97.6174 168.6947 0006820 280.1133 79.9312 14.83695242 42036
| Epoch (UTC): | 30 June 2022 20:55:52 |
| Eccentricity: | 0.0006820 |
| inclination: | 97.6174° |
| perigee height: | 613 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 168.6947° |
| argument of perigee: | 280.1133° |
| revolutions per day: | 14.83695242 |
| mean anomaly at epoch: | 79.9312° |
| orbit number at epoch: | 4203 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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