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 64926U 26145.56411503 +.00000000 +00000-0 +67728-3 0 00006
2 64926 53.1611 348.5868 0002214 106.7341 253.3903 15.31692443 02
| Epoch (UTC): | 25 May 2026 13:32:19 |
| Eccentricity: | 0.0002214 |
| inclination: | 53.1611° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 348.5868° |
| argument of perigee: | 106.7341° |
| revolutions per day: | 15.31692443 |
| mean anomaly at epoch: | 253.3903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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