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 26145.16333602 +.00000000 +00000-0 +16752-3 0 00007
2 38782 97.6145 122.6761 0016794 316.6905 43.2986 14.79970175 06
| Epoch (UTC): | 25 May 2026 03:55:12 |
| Eccentricity: | 0.0016794 |
| inclination: | 97.6145° |
| perigee height: | 618 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 122.6761° |
| argument of perigee: | 316.6905° |
| revolutions per day: | 14.79970175 |
| mean anomaly at epoch: | 43.2986° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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