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 00047U 60007C 23029.92010926 .00000461 00000-0 12521-3 0 9994
2 00047 66.6657 116.9594 0231201 321.9625 36.5343 14.42578687272604
| Epoch (UTC): | 29 January 2023 22:04:57 |
| Eccentricity: | 0.0231201 |
| inclination: | 66.6657° |
| perigee height: | 585 km |
| apogee height: | 915 km |
| right ascension of ascending node: | 116.9594° |
| argument of perigee: | 321.9625° |
| revolutions per day: | 14.42578687 |
| mean anomaly at epoch: | 36.5343° |
| orbit number at epoch: | 27260 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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