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 64871U 26145.63270905 +.00000000 +00000-0 +11711-3 0 00003
2 64871 97.6683 209.9693 0005752 332.3833 27.7081 14.94020391 07
| Epoch (UTC): | 25 May 2026 15:11:06 |
| Eccentricity: | 0.0005752 |
| inclination: | 97.6683° |
| perigee height: | 581 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 209.9693° |
| argument of perigee: | 332.3833° |
| revolutions per day: | 14.94020391 |
| mean anomaly at epoch: | 27.7081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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