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 64559U 26145.28273487 +.00000000 +00000-0 +14402-3 0 00005
2 64559 97.7698 259.2524 0001800 27.9764 332.1551 14.92405309 07
| Epoch (UTC): | 25 May 2026 06:47:08 |
| Eccentricity: | 0.0001800 |
| inclination: | 97.7698° |
| perigee height: | 589 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 259.2524° |
| argument of perigee: | 27.9764° |
| revolutions per day: | 14.92405309 |
| mean anomaly at epoch: | 332.1551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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