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 64251U 26145.52854245 +.00000000 +00000-0 +83931-3 0 00001
2 64251 42.9991 232.8618 0001092 273.2855 86.7871 15.27590406 04
| Epoch (UTC): | 25 May 2026 12:41:06 |
| Eccentricity: | 0.0001092 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 232.8618° |
| argument of perigee: | 273.2855° |
| revolutions per day: | 15.27590406 |
| mean anomaly at epoch: | 86.7871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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