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 64076U 26145.01025843 +.00000000 +00000-0 +94850-3 0 00006
2 64076 43.0011 357.9845 0001859 274.0327 86.0328 15.70859790 01
| Epoch (UTC): | 25 May 2026 00:14:46 |
| Eccentricity: | 0.0001859 |
| inclination: | 43.0011° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 357.9845° |
| argument of perigee: | 274.0327° |
| revolutions per day: | 15.70859790 |
| mean anomaly at epoch: | 86.0328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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