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 39208U 26145.47507756 +.00000000 +00000-0 +83229-4 0 00002
2 39208 98.0885 148.8294 0007018 210.2420 149.8383 14.72254182 07
| Epoch (UTC): | 25 May 2026 11:24:06 |
| Eccentricity: | 0.0007018 |
| inclination: | 98.0885° |
| perigee height: | 649 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 148.8294° |
| argument of perigee: | 210.2420° |
| revolutions per day: | 14.72254182 |
| mean anomaly at epoch: | 149.8383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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