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 64319U 26145.41889514 +.00000000 +00000-0 +13790-2 0 00006
2 64319 43.0007 286.5610 0001879 252.9406 107.1256 15.70955878 07
| Epoch (UTC): | 25 May 2026 10:03:12 |
| Eccentricity: | 0.0001879 |
| inclination: | 43.0007° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 286.5610° |
| argument of perigee: | 252.9406° |
| revolutions per day: | 15.70955878 |
| mean anomaly at epoch: | 107.1256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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