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 64929U 26144.85118259 +.00000000 +00000-0 +92737-3 0 00000
2 64929 53.1601 351.9590 0001064 86.8510 273.2613 15.30199590 05
| Epoch (UTC): | 24 May 2026 20:25:42 |
| Eccentricity: | 0.0001064 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 351.9590° |
| argument of perigee: | 86.8510° |
| revolutions per day: | 15.30199590 |
| mean anomaly at epoch: | 273.2613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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