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 67051U 26145.54804714 +.00000000 +00000-0 +80227-3 0 00005
2 67051 43.0019 324.0219 0001395 260.3320 99.7375 15.27589229 03
| Epoch (UTC): | 25 May 2026 13:09:11 |
| Eccentricity: | 0.0001395 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.0219° |
| argument of perigee: | 260.3320° |
| revolutions per day: | 15.27589229 |
| mean anomaly at epoch: | 99.7375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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