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 34713U 26138.53689183 +.00000000 +00000-0 +00000-0 0 00004
2 34713 0.0176 320.9153 0001161 278.5863 247.5413 1.00269659 09
| Epoch (UTC): | 18 May 2026 12:53:07 |
| Eccentricity: | 0.0001161 |
| inclination: | 0.0176° |
| perigee height: | 35782 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 320.9153° |
| argument of perigee: | 278.5863° |
| revolutions per day: | 1.00269659 |
| mean anomaly at epoch: | 247.5413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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