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 64077U 26145.43024965 +.00000000 +00000-0 +55458-3 0 00008
2 64077 42.9999 128.4405 0001579 273.0487 87.0184 15.27588220 03
| Epoch (UTC): | 25 May 2026 10:19:33 |
| Eccentricity: | 0.0001579 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 128.4405° |
| argument of perigee: | 273.0487° |
| revolutions per day: | 15.27588220 |
| mean anomaly at epoch: | 87.0184° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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