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 67766U 26145.53457181 +.00000000 +00000-0 +15115-3 0 00003
2 67766 51.9000 233.3129 0000525 88.6363 271.4660 14.79927758 03
| Epoch (UTC): | 25 May 2026 12:49:47 |
| Eccentricity: | 0.0000525 |
| inclination: | 51.9000° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 233.3129° |
| argument of perigee: | 88.6363° |
| revolutions per day: | 14.79927758 |
| mean anomaly at epoch: | 271.4660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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