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 47405U 26145.19155161 +.00000000 +00000-0 +32891-3 0 00006
2 47405 53.1603 66.6153 0001156 77.4160 282.6971 15.31701983 08
| Epoch (UTC): | 25 May 2026 04:35:50 |
| Eccentricity: | 0.0001156 |
| inclination: | 53.1603° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 66.6153° |
| argument of perigee: | 77.4160° |
| revolutions per day: | 15.31701983 |
| mean anomaly at epoch: | 282.6971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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