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 63404U 26145.37908191 +.00000000 +00000-0 +57213-3 0 00007
2 63404 43.0009 33.5449 0000949 274.3264 85.7479 15.27595563 01
| Epoch (UTC): | 25 May 2026 09:05:52 |
| Eccentricity: | 0.0000949 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.5449° |
| argument of perigee: | 274.3264° |
| revolutions per day: | 15.27595563 |
| mean anomaly at epoch: | 85.7479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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