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 26145.56945882 +.00000000 +00000-0 +60051-3 0 00005
2 64543 97.4284 256.8644 0334720 161.2676 200.1257 15.62285956 07
| Epoch (UTC): | 25 May 2026 13:40:01 |
| Eccentricity: | 0.0334720 |
| inclination: | 97.4284° |
| perigee height: | 155 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 256.8644° |
| argument of perigee: | 161.2676° |
| revolutions per day: | 15.62285956 |
| mean anomaly at epoch: | 200.1257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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