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 39059U 26159.85524079 +.00000000 +00000-0 +15033-3 0 00007
2 39059 82.5017 227.0723 0027189 54.3215 306.0390 12.42938909 09
| Epoch (UTC): | 08 June 2026 20:31:32 |
| Eccentricity: | 0.0027189 |
| inclination: | 82.5017° |
| perigee height: | 1473 km |
| apogee height: | 1516 km |
| right ascension of ascending node: | 227.0723° |
| argument of perigee: | 54.3215° |
| revolutions per day: | 12.42938909 |
| mean anomaly at epoch: | 306.0390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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