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 26032.49812726 +.00000000 +00000-0 +15221-3 0 00000
2 39090 98.3852 216.0961 0007571 277.4245 82.6081 14.37060008 08
| Epoch (UTC): | 01 February 2026 11:57:18 |
| Eccentricity: | 0.0007571 |
| inclination: | 98.3852° |
| perigee height: | 763 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 216.0961° |
| argument of perigee: | 277.4245° |
| revolutions per day: | 14.37060008 |
| mean anomaly at epoch: | 82.6081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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