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 26069.23814797 +.00000000 +00000-0 +80304-3 0 00000
2 14064 64.9901 18.4808 0052934 227.9095 131.7534 15.35051235 06
| Epoch (UTC): | 10 March 2026 05:42:55 |
| Eccentricity: | 0.0052934 |
| inclination: | 64.9901° |
| perigee height: | 425 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 18.4808° |
| argument of perigee: | 227.9095° |
| revolutions per day: | 15.35051235 |
| mean anomaly at epoch: | 131.7534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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