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 26104.16430624 +.00000000 +00000-0 +75273-3 0 00006
2 39762 82.4511 150.4991 0019934 210.1109 149.8826 12.42891681 09
| Epoch (UTC): | 14 April 2026 03:56:36 |
| Eccentricity: | 0.0019934 |
| inclination: | 82.4511° |
| perigee height: | 1479 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 150.4991° |
| argument of perigee: | 210.1109° |
| revolutions per day: | 12.42891681 |
| mean anomaly at epoch: | 149.8826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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