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 67211U 26145.24871641 +.00000000 +00000-0 +42047-3 0 00001
2 67211 70.0013 341.3799 0002194 264.5735 95.5174 14.98345075 01
| Epoch (UTC): | 25 May 2026 05:58:09 |
| Eccentricity: | 0.0002194 |
| inclination: | 70.0013° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 341.3799° |
| argument of perigee: | 264.5735° |
| revolutions per day: | 14.98345075 |
| mean anomaly at epoch: | 95.5174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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