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 26145.59516847 +.00000000 +00000-0 +00000-0 0 00004
2 34713 0.0181 331.6958 0001265 255.3528 287.9037 1.00271555 01
| Epoch (UTC): | 25 May 2026 14:17:02 |
| Eccentricity: | 0.0001265 |
| inclination: | 0.0181° |
| perigee height: | 35781 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 331.6958° |
| argument of perigee: | 255.3528° |
| revolutions per day: | 1.00271555 |
| mean anomaly at epoch: | 287.9037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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