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 64767U 26144.99891001 +.00000000 +00000-0 +69898-3 0 00000
2 64767 53.1592 247.6896 0001058 87.2817 272.8307 15.34405684 05
| Epoch (UTC): | 24 May 2026 23:58:25 |
| Eccentricity: | 0.0001058 |
| inclination: | 53.1592° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 247.6896° |
| argument of perigee: | 87.2817° |
| revolutions per day: | 15.34405684 |
| mean anomaly at epoch: | 272.8307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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