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 41744U 26137.60029367 +.00000000 +00000-0 +00000-0 0 00005
2 41744 4.1208 77.5686 0008727 333.3572 224.1751 1.00276969 08
| Epoch (UTC): | 17 May 2026 14:24:25 |
| Eccentricity: | 0.0008727 |
| inclination: | 4.1208° |
| perigee height: | 35748 km |
| apogee height: | 35822 km |
| right ascension of ascending node: | 77.5686° |
| argument of perigee: | 333.3572° |
| revolutions per day: | 1.00276969 |
| mean anomaly at epoch: | 224.1751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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