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 64934U 26145.37504606 +.00000000 +00000-0 +26512-3 0 00007
2 64934 97.4530 9.2722 0001082 81.6383 278.4967 15.05658312 07
| Epoch (UTC): | 25 May 2026 09:00:03 |
| Eccentricity: | 0.0001082 |
| inclination: | 97.4530° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 9.2722° |
| argument of perigee: | 81.6383° |
| revolutions per day: | 15.05658312 |
| mean anomaly at epoch: | 278.4967° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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