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 64745U 26145.40701874 +.00000000 +00000-0 +32915-3 0 00001
2 64745 53.1582 184.9771 0001202 86.3191 273.7947 15.30207437 03
| Epoch (UTC): | 25 May 2026 09:46:06 |
| Eccentricity: | 0.0001202 |
| inclination: | 53.1582° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.9771° |
| argument of perigee: | 86.3191° |
| revolutions per day: | 15.30207437 |
| mean anomaly at epoch: | 273.7947° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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