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 47311U 21002C 22026.82371855 .00005110 00000-0 22577-3 0 9995
2 47311 60.6845 174.3563 0026066 164.5324 195.6566 15.22916165 56884
| Epoch (UTC): | 26 January 2022 19:46:09 |
| Eccentricity: | 0.0026066 |
| inclination: | 60.6845° |
| perigee height: | 479 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 174.3563° |
| argument of perigee: | 164.5324° |
| revolutions per day: | 15.22916165 |
| mean anomaly at epoch: | 195.6566° |
| orbit number at epoch: | 5688 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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