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 62064U 26145.46258111 +.00000000 +00000-0 +11081-2 0 00000
2 62064 53.1577 52.6425 0001302 72.3360 287.7800 15.69753166 00
| Epoch (UTC): | 25 May 2026 11:06:07 |
| Eccentricity: | 0.0001302 |
| inclination: | 53.1577° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 52.6425° |
| argument of perigee: | 72.3360° |
| revolutions per day: | 15.69753166 |
| mean anomaly at epoch: | 287.7800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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