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 64223U 26145.43555572 +.00000000 +00000-0 +42873-3 0 00001
2 64223 53.1607 43.2816 0001240 84.4795 275.6347 15.30210026 03
| Epoch (UTC): | 25 May 2026 10:27:12 |
| Eccentricity: | 0.0001240 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.2816° |
| argument of perigee: | 84.4795° |
| revolutions per day: | 15.30210026 |
| mean anomaly at epoch: | 275.6347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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