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 26106.90119985 +.00000000 +00000-0 +55623-3 0 00001
2 39762 82.4505 148.7860 0020035 204.0529 155.9617 12.42891750 02
| Epoch (UTC): | 16 April 2026 21:37:43 |
| Eccentricity: | 0.0020035 |
| inclination: | 82.4505° |
| perigee height: | 1479 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 148.7860° |
| argument of perigee: | 204.0529° |
| revolutions per day: | 12.42891750 |
| mean anomaly at epoch: | 155.9617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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