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 is defined by the following mean orbital elements,
1 00047U 26104.30606087 +.00000000 +00000-0 +10974-3 0 00001
2 00047 66.6648 218.2555 0219442 186.7863 173.0262 14.45252438 07
| Epoch (UTC): | 14 April 2026 07:20:43 |
| Eccentricity: | 0.0219442 |
| inclination: | 66.6648° |
| perigee height: | 585 km |
| apogee height: | 897 km |
| right ascension of ascending node: | 218.2555° |
| argument of perigee: | 186.7863° |
| revolutions per day: | 14.45252438 |
| mean anomaly at epoch: | 173.0262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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