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 64226U 26145.43239293 +.00000000 +00000-0 +66255-3 0 00003
2 64226 53.1607 43.2584 0001438 84.2137 275.9028 15.30238481 09
| Epoch (UTC): | 25 May 2026 10:22:38 |
| Eccentricity: | 0.0001438 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.2584° |
| argument of perigee: | 84.2137° |
| revolutions per day: | 15.30238481 |
| mean anomaly at epoch: | 275.9028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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