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 63794U 26145.50642116 +.00000000 +00000-0 +59478-3 0 00001
2 63794 43.0011 338.4184 0000782 282.2559 77.8205 15.27589101 09
| Epoch (UTC): | 25 May 2026 12:09:14 |
| Eccentricity: | 0.0000782 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.4184° |
| argument of perigee: | 282.2559° |
| revolutions per day: | 15.27589101 |
| mean anomaly at epoch: | 77.8205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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