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 64591U 26145.56333715 +.00000000 +00000-0 +34107-3 0 00007
2 64591 97.7659 260.9339 0006194 56.8431 303.3384 14.96881130 04
| Epoch (UTC): | 25 May 2026 13:31:12 |
| Eccentricity: | 0.0006194 |
| inclination: | 97.7659° |
| perigee height: | 572 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 260.9339° |
| argument of perigee: | 56.8431° |
| revolutions per day: | 14.96881130 |
| mean anomaly at epoch: | 303.3384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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