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 64336U 26145.12392977 +.00000000 +00000-0 +51923-3 0 00006
2 64336 43.0036 46.2714 0001529 254.0267 106.0416 15.27600957 07
| Epoch (UTC): | 25 May 2026 02:58:27 |
| Eccentricity: | 0.0001529 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 46.2714° |
| argument of perigee: | 254.0267° |
| revolutions per day: | 15.27600957 |
| mean anomaly at epoch: | 106.0416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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