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 64859U 26145.32184997 +.00000000 +00000-0 +27882-3 0 00006
2 64859 97.4508 0.7402 0002374 90.1575 269.9924 15.05657384 08
| Epoch (UTC): | 25 May 2026 07:43:27 |
| Eccentricity: | 0.0002374 |
| inclination: | 97.4508° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.7402° |
| argument of perigee: | 90.1575° |
| revolutions per day: | 15.05657384 |
| mean anomaly at epoch: | 269.9924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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