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 39090U 26044.47387303 +.00000000 +00000-0 +15301-3 0 00008
2 39090 98.3861 227.7703 0007743 236.6780 123.3666 14.37072594 08
| Epoch (UTC): | 13 February 2026 11:22:22 |
| Eccentricity: | 0.0007743 |
| inclination: | 98.3861° |
| perigee height: | 763 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 227.7703° |
| argument of perigee: | 236.6780° |
| revolutions per day: | 14.37072594 |
| mean anomaly at epoch: | 123.3666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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