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 38778U 26145.58936178 +.00000000 +00000-0 +00000-0 0 00001
2 38778 0.0335 255.3112 0000888 270.7521 317.4772 1.00273686 07
| Epoch (UTC): | 25 May 2026 14:08:40 |
| Eccentricity: | 0.0000888 |
| inclination: | 0.0335° |
| perigee height: | 35782 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 255.3112° |
| argument of perigee: | 270.7521° |
| revolutions per day: | 1.00273686 |
| mean anomaly at epoch: | 317.4772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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