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 64452U 26145.55203990 +.00000000 +00000-0 +10790-1 0 00003
2 64452 53.1578 91.3276 0003399 128.7485 231.3820 15.29856256 07
| Epoch (UTC): | 25 May 2026 13:14:56 |
| Eccentricity: | 0.0003399 |
| inclination: | 53.1578° |
| perigee height: | 474 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 91.3276° |
| argument of perigee: | 128.7485° |
| revolutions per day: | 15.29856256 |
| mean anomaly at epoch: | 231.3820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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