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 67786U 26145.41180737 +.00000000 +00000-0 +23223-3 0 00001
2 67786 51.8980 218.4705 0001513 103.9774 256.1355 14.76356843 09
| Epoch (UTC): | 25 May 2026 09:53:00 |
| Eccentricity: | 0.0001513 |
| inclination: | 51.8980° |
| perigee height: | 640 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 218.4705° |
| argument of perigee: | 103.9774° |
| revolutions per day: | 14.76356843 |
| mean anomaly at epoch: | 256.1355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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