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 35934U 26031.67065584 +.00000000 +00000-0 +22856-3 0 00006
2 35934 98.4152 293.2426 0005241 317.2001 42.8790 14.59952195 09
| Epoch (UTC): | 31 January 2026 16:05:44 |
| Eccentricity: | 0.0005241 |
| inclination: | 98.4152° |
| perigee height: | 690 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 293.2426° |
| argument of perigee: | 317.2001° |
| revolutions per day: | 14.59952195 |
| mean anomaly at epoch: | 42.8790° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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