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 64339U 26145.08119059 +.00000000 +00000-0 +34231-3 0 00005
2 64339 42.9991 50.2692 0001334 259.3283 100.7419 15.27590494 06
| Epoch (UTC): | 25 May 2026 01:56:54 |
| Eccentricity: | 0.0001334 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 50.2692° |
| argument of perigee: | 259.3283° |
| revolutions per day: | 15.27590494 |
| mean anomaly at epoch: | 100.7419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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