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 63422U 26145.41890081 +.00000000 +00000-0 +46481-3 0 00005
2 63422 43.0049 33.7812 0001126 280.6750 79.3975 15.27596065 07
| Epoch (UTC): | 25 May 2026 10:03:13 |
| Eccentricity: | 0.0001126 |
| inclination: | 43.0049° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.7812° |
| argument of perigee: | 280.6750° |
| revolutions per day: | 15.27596065 |
| mean anomaly at epoch: | 79.3975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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