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 47747U 26145.38274751 +.00000000 +00000-0 +37285-4 0 00006
2 47747 53.1582 197.1921 0001211 85.2478 274.8662 15.31703842 03
| Epoch (UTC): | 25 May 2026 09:11:09 |
| Eccentricity: | 0.0001211 |
| inclination: | 53.1582° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 197.1921° |
| argument of perigee: | 85.2478° |
| revolutions per day: | 15.31703842 |
| mean anomaly at epoch: | 274.8662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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