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 63473U 26145.57424440 +.00000000 +00000-0 +23946-3 0 00001
2 63473 43.0026 185.7083 0001466 268.5276 91.5408 15.27580837 08
| Epoch (UTC): | 25 May 2026 13:46:54 |
| Eccentricity: | 0.0001466 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.7083° |
| argument of perigee: | 268.5276° |
| revolutions per day: | 15.27580837 |
| mean anomaly at epoch: | 91.5408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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