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 64229U 26145.43155420 +.00000000 +00000-0 +91394-3 0 00007
2 64229 53.1600 43.3165 0001611 96.4861 263.6325 15.33568507 05
| Epoch (UTC): | 25 May 2026 10:21:26 |
| Eccentricity: | 0.0001611 |
| inclination: | 53.1600° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 43.3165° |
| argument of perigee: | 96.4861° |
| revolutions per day: | 15.33568507 |
| mean anomaly at epoch: | 263.6325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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