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 67047U 26145.47623412 +.00000000 +00000-0 +81744-3 0 00001
2 67047 43.0008 324.3446 0001234 274.1297 85.9413 15.27595328 06
| Epoch (UTC): | 25 May 2026 11:25:46 |
| Eccentricity: | 0.0001234 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.3446° |
| argument of perigee: | 274.1297° |
| revolutions per day: | 15.27595328 |
| mean anomaly at epoch: | 85.9413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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