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 67067U 26145.61110801 +.00000000 +00000-0 +88818-4 0 00002
2 67067 49.9999 106.1224 0000865 355.4569 4.6295 13.29327519 07
| Epoch (UTC): | 25 May 2026 14:39:59 |
| Eccentricity: | 0.0000865 |
| inclination: | 49.9999° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 106.1224° |
| argument of perigee: | 355.4569° |
| revolutions per day: | 13.29327519 |
| mean anomaly at epoch: | 4.6295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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