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 67520U 26145.57764847 +.00000000 +00000-0 +47614-3 0 00004
2 67520 43.0017 239.9312 0001054 270.5575 89.5156 15.27586238 08
| Epoch (UTC): | 25 May 2026 13:51:48 |
| Eccentricity: | 0.0001054 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 239.9312° |
| argument of perigee: | 270.5575° |
| revolutions per day: | 15.27586238 |
| mean anomaly at epoch: | 89.5156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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