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 39762U 26145.62016052 +.00000000 +00000-0 +47228-3 0 00006
2 39762 82.4477 124.5471 0021524 120.8916 239.4283 12.42893375 01
| Epoch (UTC): | 25 May 2026 14:53:01 |
| Eccentricity: | 0.0021524 |
| inclination: | 82.4477° |
| perigee height: | 1477 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 124.5471° |
| argument of perigee: | 120.8916° |
| revolutions per day: | 12.42893375 |
| mean anomaly at epoch: | 239.4283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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