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 64125U 26145.53387780 +.00000000 +00000-0 +15685-2 0 00007
2 64125 42.9985 230.7519 0000662 275.2001 84.8791 15.70900142 01
| Epoch (UTC): | 25 May 2026 12:48:47 |
| Eccentricity: | 0.0000662 |
| inclination: | 42.9985° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 230.7519° |
| argument of perigee: | 275.2001° |
| revolutions per day: | 15.70900142 |
| mean anomaly at epoch: | 84.8791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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