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 26108.25058619 +.00000000 +00000-0 +10874-3 0 00000
2 00047 66.6646 207.6549 0219054 183.9065 176.0342 14.45256305 01
| Epoch (UTC): | 18 April 2026 06:00:50 |
| Eccentricity: | 0.0219054 |
| inclination: | 66.6646° |
| perigee height: | 585 km |
| apogee height: | 897 km |
| right ascension of ascending node: | 207.6549° |
| argument of perigee: | 183.9065° |
| revolutions per day: | 14.45256305 |
| mean anomaly at epoch: | 176.0342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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