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 39092U 26106.78147394 +.00000000 +00000-0 +49541-4 0 00001
2 39092 98.4021 287.8364 0010180 63.8529 296.3704 14.36388064 04
| Epoch (UTC): | 16 April 2026 18:45:19 |
| Eccentricity: | 0.0010180 |
| inclination: | 98.4021° |
| perigee height: | 763 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 287.8364° |
| argument of perigee: | 63.8529° |
| revolutions per day: | 14.36388064 |
| mean anomaly at epoch: | 296.3704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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