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 26146.02290454 +.00000000 +00000-0 +00000-0 0 00006
2 34713 0.0177 334.0505 0001247 251.0312 84.2764 1.00271651 07
| Epoch (UTC): | 26 May 2026 00:32:58 |
| Eccentricity: | 0.0001247 |
| inclination: | 0.0177° |
| perigee height: | 35781 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 334.0505° |
| argument of perigee: | 251.0312° |
| revolutions per day: | 1.00271651 |
| mean anomaly at epoch: | 84.2764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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