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 62862U 26145.38574236 +.00000000 +00000-0 +10438-2 0 00001
2 62862 53.1571 133.2849 0001175 89.3964 270.7171 15.30203901 00
| Epoch (UTC): | 25 May 2026 09:15:28 |
| Eccentricity: | 0.0001175 |
| inclination: | 53.1571° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.2849° |
| argument of perigee: | 89.3964° |
| revolutions per day: | 15.30203901 |
| mean anomaly at epoch: | 270.7171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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