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 67785U 26145.37895700 +.00000000 +00000-0 -54926-4 0 00004
2 67785 51.8887 214.7007 0018792 342.0758 17.9558 15.23524193 09
| Epoch (UTC): | 25 May 2026 09:05:41 |
| Eccentricity: | 0.0018792 |
| inclination: | 51.8887° |
| perigee height: | 482 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 214.7007° |
| argument of perigee: | 342.0758° |
| revolutions per day: | 15.23524193 |
| mean anomaly at epoch: | 17.9558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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