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 64279U 26145.33885539 +.00000000 +00000-0 +11131-2 0 00002
2 64279 53.1591 118.3768 0001450 72.9693 287.1469 15.35402484 07
| Epoch (UTC): | 25 May 2026 08:07:57 |
| Eccentricity: | 0.0001450 |
| inclination: | 53.1591° |
| perigee height: | 459 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 118.3768° |
| argument of perigee: | 72.9693° |
| revolutions per day: | 15.35402484 |
| mean anomaly at epoch: | 287.1469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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