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 26069.95478095 +.00000000 +00000-0 +73787-3 0 00003
2 14064 64.9900 16.1163 0052943 227.6568 132.0078 15.35092919 07
| Epoch (UTC): | 10 March 2026 22:54:53 |
| Eccentricity: | 0.0052943 |
| inclination: | 64.9900° |
| perigee height: | 424 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 16.1163° |
| argument of perigee: | 227.6568° |
| revolutions per day: | 15.35092919 |
| mean anomaly at epoch: | 132.0078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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