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 66533U 26145.45528309 +.00000000 +00000-0 +49636-3 0 00001
2 66533 42.9996 204.4105 0001471 273.4671 86.6012 15.27589656 00
| Epoch (UTC): | 25 May 2026 10:55:36 |
| Eccentricity: | 0.0001471 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.4105° |
| argument of perigee: | 273.4671° |
| revolutions per day: | 15.27589656 |
| mean anomaly at epoch: | 86.6012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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