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 64543U 26071.69546442 +.00000000 +00000-0 +61456-3 0 00006
2 64543 97.4466 184.8633 0406504 56.3071 307.6220 15.00542457 07
| Epoch (UTC): | 12 March 2026 16:41:28 |
| Eccentricity: | 0.0406504 |
| inclination: | 97.4466° |
| perigee height: | 283 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 184.8633° |
| argument of perigee: | 56.3071° |
| revolutions per day: | 15.00542457 |
| mean anomaly at epoch: | 307.6220° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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