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 23159.49960005 .00001509 00000-0 18346-3 0 9999
2 14781 97.6568 136.7670 0006949 222.5266 137.5412 14.84878567 92852
| Epoch (UTC): | 08 June 2023 11:59:25 |
| Eccentricity: | 0.0006949 |
| inclination: | 97.6568° |
| perigee height: | 609 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 136.7670° |
| argument of perigee: | 222.5266° |
| revolutions per day: | 14.84878567 |
| mean anomaly at epoch: | 137.5412° |
| orbit number at epoch: | 9285 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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