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 67911U 26145.46578086 +.00000000 +00000-0 +35083-3 0 00001
2 67911 43.0043 171.6939 0001569 268.0222 92.0450 15.27589408 08
| Epoch (UTC): | 25 May 2026 11:10:43 |
| Eccentricity: | 0.0001569 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.6939° |
| argument of perigee: | 268.0222° |
| revolutions per day: | 15.27589408 |
| mean anomaly at epoch: | 92.0450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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