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 63661U 26145.44057927 +.00000000 +00000-0 +78167-3 0 00003
2 63661 43.0001 291.8692 0000757 290.7191 69.3580 15.27591539 05
| Epoch (UTC): | 25 May 2026 10:34:26 |
| Eccentricity: | 0.0000757 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 291.8692° |
| argument of perigee: | 290.7191° |
| revolutions per day: | 15.27591539 |
| mean anomaly at epoch: | 69.3580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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