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 39084U 26039.81930139 +.00000000 +00000-0 +11365-3 0 00000
2 39084 98.1977 112.0094 0001287 92.6591 267.4755 14.57119997 03
| Epoch (UTC): | 08 February 2026 19:39:47 |
| Eccentricity: | 0.0001287 |
| inclination: | 98.1977° |
| perigee height: | 702 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 112.0094° |
| argument of perigee: | 92.6591° |
| revolutions per day: | 14.57119997 |
| mean anomaly at epoch: | 267.4755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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