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 63278U 26145.53937972 +.00000000 +00000-0 +55893-3 0 00005
2 63278 43.0001 168.0285 0001408 275.5935 84.4756 15.27595952 09
| Epoch (UTC): | 25 May 2026 12:56:42 |
| Eccentricity: | 0.0001408 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 168.0285° |
| argument of perigee: | 275.5935° |
| revolutions per day: | 15.27595952 |
| mean anomaly at epoch: | 84.4756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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