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 66641U 26145.31625366 +.00000000 +00000-0 +52730-3 0 00006
2 66641 53.1592 144.3531 0001233 83.5978 276.5163 15.30208749 09
| Epoch (UTC): | 25 May 2026 07:35:24 |
| Eccentricity: | 0.0001233 |
| inclination: | 53.1592° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 144.3531° |
| argument of perigee: | 83.5978° |
| revolutions per day: | 15.30208749 |
| mean anomaly at epoch: | 276.5163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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