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 61964U 26144.90523784 +.00000000 +00000-0 +46500-3 0 00002
2 61964 42.9983 94.9088 0000197 109.8469 250.2404 15.27593428 08
| Epoch (UTC): | 24 May 2026 21:43:32 |
| Eccentricity: | 0.0000197 |
| inclination: | 42.9983° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 94.9088° |
| argument of perigee: | 109.8469° |
| revolutions per day: | 15.27593428 |
| mean anomaly at epoch: | 250.2404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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