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 63424U 26145.37664767 +.00000000 +00000-0 +94995-3 0 00005
2 63424 43.0008 34.3153 0001268 265.0002 95.0705 15.27588968 02
| Epoch (UTC): | 25 May 2026 09:02:22 |
| Eccentricity: | 0.0001268 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 34.3153° |
| argument of perigee: | 265.0002° |
| revolutions per day: | 15.27588968 |
| mean anomaly at epoch: | 95.0705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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