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 26160.19005205 +.00000000 +00000-0 +45576-3 0 00007
2 39762 82.4492 115.4266 0021838 90.5771 269.7811 12.42893966 08
| Epoch (UTC): | 09 June 2026 04:33:40 |
| Eccentricity: | 0.0021838 |
| inclination: | 82.4492° |
| perigee height: | 1477 km |
| apogee height: | 1512 km |
| right ascension of ascending node: | 115.4266° |
| argument of perigee: | 90.5771° |
| revolutions per day: | 12.42893966 |
| mean anomaly at epoch: | 269.7811° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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