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 67636U 26145.49168042 +.00000000 +00000-0 +69526-3 0 00004
2 67636 43.0030 65.6637 0000469 280.2286 79.8513 15.27591636 08
| Epoch (UTC): | 25 May 2026 11:48:01 |
| Eccentricity: | 0.0000469 |
| inclination: | 43.0030° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 65.6637° |
| argument of perigee: | 280.2286° |
| revolutions per day: | 15.27591636 |
| mean anomaly at epoch: | 79.8513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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