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 47904U 26145.28117778 +.00000000 +00000-0 +16149-3 0 00000
2 47904 53.1559 259.0292 0001082 84.6812 275.4312 15.31706330 06
| Epoch (UTC): | 25 May 2026 06:44:53 |
| Eccentricity: | 0.0001082 |
| inclination: | 53.1559° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 259.0292° |
| argument of perigee: | 84.6812° |
| revolutions per day: | 15.31706330 |
| mean anomaly at epoch: | 275.4312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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