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 39088U 26145.57418495 +.00000000 +00000-0 +46703-4 0 00006
2 39088 98.4257 325.5679 0010383 321.4117 38.6326 14.35233450 04
| Epoch (UTC): | 25 May 2026 13:46:49 |
| Eccentricity: | 0.0010383 |
| inclination: | 98.4257° |
| perigee height: | 767 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 325.5679° |
| argument of perigee: | 321.4117° |
| revolutions per day: | 14.35233450 |
| mean anomaly at epoch: | 38.6326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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