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 64679U 26145.37208007 +.00000000 +00000-0 +87678-3 0 00009
2 64679 53.1589 130.2107 0001272 93.2678 266.8470 15.34407947 03
| Epoch (UTC): | 25 May 2026 08:55:47 |
| Eccentricity: | 0.0001272 |
| inclination: | 53.1589° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 130.2107° |
| argument of perigee: | 93.2678° |
| revolutions per day: | 15.34407947 |
| mean anomaly at epoch: | 266.8470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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