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 67669U 26145.36189297 +.00000000 +00000-0 +77815-3 0 00001
2 67669 97.2850 178.6258 0000108 334.2894 25.8343 15.33450787 04
| Epoch (UTC): | 25 May 2026 08:41:07 |
| Eccentricity: | 0.0000108 |
| inclination: | 97.2850° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.6258° |
| argument of perigee: | 334.2894° |
| revolutions per day: | 15.33450787 |
| mean anomaly at epoch: | 25.8343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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