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 62149U 26145.53950108 +.00000000 +00000-0 +55038-3 0 00008
2 62149 43.0030 84.0598 0001392 251.9003 108.1697 15.27610732 09
| Epoch (UTC): | 25 May 2026 12:56:52 |
| Eccentricity: | 0.0001392 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 84.0598° |
| argument of perigee: | 251.9003° |
| revolutions per day: | 15.27610732 |
| mean anomaly at epoch: | 108.1697° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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