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 38665U 26086.31048313 +.00000000 +00000-0 +70326-4 0 00008
2 38665 74.0451 99.6241 0031280 240.0888 119.7159 14.38218527 00
| Epoch (UTC): | 27 March 2026 07:27:05 |
| Eccentricity: | 0.0031280 |
| inclination: | 74.0451° |
| perigee height: | 742 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 99.6241° |
| argument of perigee: | 240.0888° |
| revolutions per day: | 14.38218527 |
| mean anomaly at epoch: | 119.7159° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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