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 39429U 26157.11197075 +.00000000 +00000-0 +58002-3 0 00000
2 39429 97.6640 17.5254 0115274 61.0456 300.2255 14.76197048 01
| Epoch (UTC): | 06 June 2026 02:41:14 |
| Eccentricity: | 0.0115274 |
| inclination: | 97.6640° |
| perigee height: | 560 km |
| apogee height: | 722 km |
| right ascension of ascending node: | 17.5254° |
| argument of perigee: | 61.0456° |
| revolutions per day: | 14.76197048 |
| mean anomaly at epoch: | 300.2255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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