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 64743U 26145.38169289 +.00000000 +00000-0 +38417-3 0 00007
2 64743 53.1590 184.8187 0001124 86.8978 273.2151 15.30205707 01
| Epoch (UTC): | 25 May 2026 09:09:38 |
| Eccentricity: | 0.0001124 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.8187° |
| argument of perigee: | 86.8978° |
| revolutions per day: | 15.30205707 |
| mean anomaly at epoch: | 273.2151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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