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 63478U 26145.54518845 +.00000000 +00000-0 +15750-3 0 00000
2 63478 43.0015 182.0044 0001547 278.5457 81.5219 15.27552585 08
| Epoch (UTC): | 25 May 2026 13:05:04 |
| Eccentricity: | 0.0001547 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 182.0044° |
| argument of perigee: | 278.5457° |
| revolutions per day: | 15.27552585 |
| mean anomaly at epoch: | 81.5219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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