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 37258U 26145.15774905 +.00000000 +00000-0 +00000-0 0 00004
2 37258 0.0622 11.3871 0003671 114.1129 183.0249 1.00270746 08
| Epoch (UTC): | 25 May 2026 03:47:09 |
| Eccentricity: | 0.0003671 |
| inclination: | 0.0622° |
| perigee height: | 35771 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 11.3871° |
| argument of perigee: | 114.1129° |
| revolutions per day: | 1.00270746 |
| mean anomaly at epoch: | 183.0249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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