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 34492U 26017.82757979 +.00000000 +00000-0 +26496-2 0 00004
2 34492 86.4718 320.0336 0190508 121.5498 269.3758 14.26380248 06
| Epoch (UTC): | 17 January 2026 19:51:42 |
| Eccentricity: | 0.0190508 |
| inclination: | 86.4718° |
| perigee height: | 667 km |
| apogee height: | 941 km |
| right ascension of ascending node: | 320.0336° |
| argument of perigee: | 121.5498° |
| revolutions per day: | 14.26380248 |
| mean anomaly at epoch: | 269.3758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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