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 67775U 26145.51696404 +.00000000 +00000-0 +22890-3 0 00002
2 67775 51.8968 229.6417 0006992 326.9658 33.0865 14.76530687 09
| Epoch (UTC): | 25 May 2026 12:24:25 |
| Eccentricity: | 0.0006992 |
| inclination: | 51.8968° |
| perigee height: | 635 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 229.6417° |
| argument of perigee: | 326.9658° |
| revolutions per day: | 14.76530687 |
| mean anomaly at epoch: | 33.0865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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