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 64156U 26145.56396605 +.00000000 +00000-0 +36688-3 0 00007
2 64156 97.4484 196.8929 0001096 157.0584 203.0692 15.05660342 04
| Epoch (UTC): | 25 May 2026 13:32:06 |
| Eccentricity: | 0.0001096 |
| inclination: | 97.4484° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 196.8929° |
| argument of perigee: | 157.0584° |
| revolutions per day: | 15.05660342 |
| mean anomaly at epoch: | 203.0692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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