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 46685U 26145.60440922 +.00000000 +00000-0 +67819-3 0 00001
2 46685 53.0445 226.7349 0003147 304.6914 55.3806 15.69972634 06
| Epoch (UTC): | 25 May 2026 14:30:20 |
| Eccentricity: | 0.0003147 |
| inclination: | 53.0445° |
| perigee height: | 357 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 226.7349° |
| argument of perigee: | 304.6914° |
| revolutions per day: | 15.69972634 |
| mean anomaly at epoch: | 55.3806° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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