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 38782U 26145.56899771 +.00000000 +00000-0 +16645-3 0 00006
2 38782 97.6144 123.0607 0016757 315.2712 44.7149 14.79971116 02
| Epoch (UTC): | 25 May 2026 13:39:21 |
| Eccentricity: | 0.0016757 |
| inclination: | 97.6144° |
| perigee height: | 618 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 123.0607° |
| argument of perigee: | 315.2712° |
| revolutions per day: | 14.79971116 |
| mean anomaly at epoch: | 44.7149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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