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 63423U 26145.38678455 +.00000000 +00000-0 +80407-3 0 00007
2 63423 43.0005 33.5405 0000974 257.1118 102.9625 15.27583979 08
| Epoch (UTC): | 25 May 2026 09:16:58 |
| Eccentricity: | 0.0000974 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.5405° |
| argument of perigee: | 257.1118° |
| revolutions per day: | 15.27583979 |
| mean anomaly at epoch: | 102.9625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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