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 67180U 26145.30631769 +.00000000 +00000-0 +20809-3 0 00000
2 67180 43.0031 237.9404 0001456 271.5779 88.4906 15.27583255 06
| Epoch (UTC): | 25 May 2026 07:21:05 |
| Eccentricity: | 0.0001456 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 237.9404° |
| argument of perigee: | 271.5779° |
| revolutions per day: | 15.27583255 |
| mean anomaly at epoch: | 88.4906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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