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 64431U 26145.56047175 +.00000000 +00000-0 +25571-3 0 00007
2 64431 70.0006 240.5606 0003723 269.9965 90.0767 14.98338851 06
| Epoch (UTC): | 25 May 2026 13:27:04 |
| Eccentricity: | 0.0003723 |
| inclination: | 70.0006° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 240.5606° |
| argument of perigee: | 269.9965° |
| revolutions per day: | 14.98338851 |
| mean anomaly at epoch: | 90.0767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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