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 64446U 26145.27807625 +.00000000 +00000-0 +40738-3 0 00007
2 64446 53.1580 92.4694 0001268 94.5228 265.5918 15.30211745 04
| Epoch (UTC): | 25 May 2026 06:40:25 |
| Eccentricity: | 0.0001268 |
| inclination: | 53.1580° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 92.4694° |
| argument of perigee: | 94.5228° |
| revolutions per day: | 15.30211745 |
| mean anomaly at epoch: | 265.5918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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