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 64727U 26145.53553867 +.00000000 +00000-0 +35664-3 0 00006
2 64727 53.1575 184.3634 0001170 75.5216 284.5915 15.30203100 07
| Epoch (UTC): | 25 May 2026 12:51:10 |
| Eccentricity: | 0.0001170 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.3634° |
| argument of perigee: | 75.5216° |
| revolutions per day: | 15.30203100 |
| mean anomaly at epoch: | 284.5915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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