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 26106.25722514 +.00000000 +00000-0 +40345-4 0 00003
2 39762 82.4507 149.1891 0020004 205.4593 154.5503 12.42891394 08
| Epoch (UTC): | 16 April 2026 06:10:24 |
| Eccentricity: | 0.0020004 |
| inclination: | 82.4507° |
| perigee height: | 1479 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 149.1891° |
| argument of perigee: | 205.4593° |
| revolutions per day: | 12.42891394 |
| mean anomaly at epoch: | 154.5503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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