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 47408U 26145.66668980 +.00000000 +00000-0 +16819-2 0 00000
2 47408 53.1586 39.1665 0001294 115.1072 227.5614 15.31662865 06
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001294 |
| inclination: | 53.1586° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 39.1665° |
| argument of perigee: | 115.1072° |
| revolutions per day: | 15.31662865 |
| mean anomaly at epoch: | 227.5614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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