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 46706U 26145.42694410 +.00000000 +00000-0 +12745-2 0 00005
2 46706 53.0589 232.8936 0003365 6.4212 353.6830 15.29703590 09
| Epoch (UTC): | 25 May 2026 10:14:47 |
| Eccentricity: | 0.0003365 |
| inclination: | 53.0589° |
| perigee height: | 474 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 232.8936° |
| argument of perigee: | 6.4212° |
| revolutions per day: | 15.29703590 |
| mean anomaly at epoch: | 353.6830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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