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 67447U 26145.30533176 +.00000000 +00000-0 +89776-3 0 00007
2 67447 43.0003 132.1819 0000967 268.9009 91.1732 15.27546603 03
| Epoch (UTC): | 25 May 2026 07:19:40 |
| Eccentricity: | 0.0000967 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.1819° |
| argument of perigee: | 268.9009° |
| revolutions per day: | 15.27546603 |
| mean anomaly at epoch: | 91.1732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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