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 64910U 26144.86025003 +.00000000 +00000-0 +68433-3 0 00001
2 64910 53.1583 351.3120 0000458 348.6610 11.4381 15.31701210 06
| Epoch (UTC): | 24 May 2026 20:38:45 |
| Eccentricity: | 0.0000458 |
| inclination: | 53.1583° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 351.3120° |
| argument of perigee: | 348.6610° |
| revolutions per day: | 15.31701210 |
| mean anomaly at epoch: | 11.4381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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