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 64612U 26145.54856024 +.00000000 +00000-0 +86649-3 0 00000
2 64612 53.1591 338.1342 0001123 60.4484 299.6629 15.30214762 06
| Epoch (UTC): | 25 May 2026 13:09:55 |
| Eccentricity: | 0.0001123 |
| inclination: | 53.1591° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.1342° |
| argument of perigee: | 60.4484° |
| revolutions per day: | 15.30214762 |
| mean anomaly at epoch: | 299.6629° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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