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 62107U 26145.41056608 +.00000000 +00000-0 +75375-3 0 00007
2 62107 43.0030 132.3508 0001910 255.3435 104.7205 15.27596326 03
| Epoch (UTC): | 25 May 2026 09:51:12 |
| Eccentricity: | 0.0001910 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.3508° |
| argument of perigee: | 255.3435° |
| revolutions per day: | 15.27596326 |
| mean anomaly at epoch: | 104.7205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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