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 66833U 26145.44250602 +.00000000 +00000-0 +35883-3 0 00000
2 66833 70.0006 140.8995 0004021 268.0037 92.0662 14.98332115 02
| Epoch (UTC): | 25 May 2026 10:37:12 |
| Eccentricity: | 0.0004021 |
| inclination: | 70.0006° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 140.8995° |
| argument of perigee: | 268.0037° |
| revolutions per day: | 14.98332115 |
| mean anomaly at epoch: | 92.0662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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