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 63411U 26144.99750602 +.00000000 +00000-0 +98247-3 0 00006
2 63411 42.9995 43.6200 0001174 276.5865 83.4853 15.27601708 00
| Epoch (UTC): | 24 May 2026 23:56:24 |
| Eccentricity: | 0.0001174 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 43.6200° |
| argument of perigee: | 276.5865° |
| revolutions per day: | 15.27601708 |
| mean anomaly at epoch: | 83.4853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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