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 46727U 26145.48220757 +.00000000 +00000-0 +61129-3 0 00004
2 46727 53.0365 167.5756 0006770 356.2726 3.8239 15.69013869 01
| Epoch (UTC): | 25 May 2026 11:34:22 |
| Eccentricity: | 0.0006770 |
| inclination: | 53.0365° |
| perigee height: | 357 km |
| apogee height: | 366 km |
| right ascension of ascending node: | 167.5756° |
| argument of perigee: | 356.2726° |
| revolutions per day: | 15.69013869 |
| mean anomaly at epoch: | 3.8239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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