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 29713U 26022.29229471 +.00000000 +00000-0 +48057-3 0 00000
2 29713 98.0357 50.4779 0018525 224.6700 135.3029 14.97600572 04
| Epoch (UTC): | 22 January 2026 07:00:54 |
| Eccentricity: | 0.0018525 |
| inclination: | 98.0357° |
| perigee height: | 561 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 50.4779° |
| argument of perigee: | 224.6700° |
| revolutions per day: | 14.97600572 |
| mean anomaly at epoch: | 135.3029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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