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 64923U 26145.26100396 +.00000000 +00000-0 +76349-3 0 00004
2 64923 53.1594 350.2481 0000765 44.2626 315.8436 15.30217596 07
| Epoch (UTC): | 25 May 2026 06:15:50 |
| Eccentricity: | 0.0000765 |
| inclination: | 53.1594° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 350.2481° |
| argument of perigee: | 44.2626° |
| revolutions per day: | 15.30217596 |
| mean anomaly at epoch: | 315.8436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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