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 47407U 26145.60050953 +.00000000 +00000-0 -35195-5 0 00000
2 47407 53.1586 41.0846 0001278 99.3668 260.7478 15.31697349 06
| Epoch (UTC): | 25 May 2026 14:24:44 |
| Eccentricity: | 0.0001278 |
| inclination: | 53.1586° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 41.0846° |
| argument of perigee: | 99.3668° |
| revolutions per day: | 15.31697349 |
| mean anomaly at epoch: | 260.7478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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