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 14064U 26066.17595295 +.00000000 +00000-0 +72245-3 0 00004
2 14064 64.9899 28.5818 0053181 229.1470 130.5051 15.34867865 05
| Epoch (UTC): | 07 March 2026 04:13:22 |
| Eccentricity: | 0.0053181 |
| inclination: | 64.9899° |
| perigee height: | 425 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 28.5818° |
| argument of perigee: | 229.1470° |
| revolutions per day: | 15.34867865 |
| mean anomaly at epoch: | 130.5051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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