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 64467U 26145.74575644 +.00000000 +00000-0 +00000-0 0 00000
2 64467 0.0512 54.2826 0001084 100.3904 95.1442 1.00272289 00
| Epoch (UTC): | 25 May 2026 17:53:53 |
| Eccentricity: | 0.0001084 |
| inclination: | 0.0512° |
| perigee height: | 35782 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 54.2826° |
| argument of perigee: | 100.3904° |
| revolutions per day: | 1.00272289 |
| mean anomaly at epoch: | 95.1442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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