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 63064U 26145.36281691 +.00000000 +00000-0 +12847-2 0 00000
2 63064 43.0001 272.8118 0000904 184.8491 175.2368 15.70960291 08
| Epoch (UTC): | 25 May 2026 08:42:27 |
| Eccentricity: | 0.0000904 |
| inclination: | 43.0001° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 272.8118° |
| argument of perigee: | 184.8491° |
| revolutions per day: | 15.70960291 |
| mean anomaly at epoch: | 175.2368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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