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 67947U 26145.31481961 +.00000000 +00000-0 +61567-3 0 00005
2 67947 43.0049 117.6279 0002209 280.7509 79.3094 15.27601475 02
| Epoch (UTC): | 25 May 2026 07:33:20 |
| Eccentricity: | 0.0002209 |
| inclination: | 43.0049° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 117.6279° |
| argument of perigee: | 280.7509° |
| revolutions per day: | 15.27601475 |
| mean anomaly at epoch: | 79.3094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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