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 26145.60786333 +.00000000 +00000-0 -33136-3 0 00003
2 39059 82.5022 235.9289 0027499 84.3190 276.1024 12.42938274 05
| Epoch (UTC): | 25 May 2026 14:35:19 |
| Eccentricity: | 0.0027499 |
| inclination: | 82.5022° |
| perigee height: | 1473 km |
| apogee height: | 1516 km |
| right ascension of ascending node: | 235.9289° |
| argument of perigee: | 84.3190° |
| revolutions per day: | 12.42938274 |
| mean anomaly at epoch: | 276.1024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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