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 46689U 26145.58335647 +.00000000 +00000-0 +11506-2 0 00000
2 46689 53.0361 197.8064 0007306 354.4482 162.8432 15.79148386 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0007306 |
| inclination: | 53.0361° |
| perigee height: | 328 km |
| apogee height: | 338 km |
| right ascension of ascending node: | 197.8064° |
| argument of perigee: | 354.4482° |
| revolutions per day: | 15.79148386 |
| mean anomaly at epoch: | 162.8432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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