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 46687U 26145.58335647 +.00000000 +00000-0 +87783-3 0 00009
2 46687 53.0391 166.3892 0004569 33.8832 283.5830 15.78223844 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0004569 |
| inclination: | 53.0391° |
| perigee height: | 332 km |
| apogee height: | 339 km |
| right ascension of ascending node: | 166.3892° |
| argument of perigee: | 33.8832° |
| revolutions per day: | 15.78223844 |
| mean anomaly at epoch: | 283.5830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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