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 64256U 26145.40014068 +.00000000 +00000-0 +70716-3 0 00001
2 64256 53.1590 118.0602 0000610 86.3429 273.7644 15.35441086 05
| Epoch (UTC): | 25 May 2026 09:36:12 |
| Eccentricity: | 0.0000610 |
| inclination: | 53.1590° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 118.0602° |
| argument of perigee: | 86.3429° |
| revolutions per day: | 15.35441086 |
| mean anomaly at epoch: | 273.7644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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