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 26098.29628191 +.00000000 +00000-0 +00000-0 0 00004
2 34713 0.0123 207.7095 0000374 255.0621 257.9491 1.00270674 05
| Epoch (UTC): | 08 April 2026 07:06:38 |
| Eccentricity: | 0.0000374 |
| inclination: | 0.0123° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 207.7095° |
| argument of perigee: | 255.0621° |
| revolutions per day: | 1.00270674 |
| mean anomaly at epoch: | 257.9491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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