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 11239U 26022.20049718 +.00000000 +00000-0 +91405-4 0 00005
2 11239 82.9378 276.7769 0039367 258.0712 216.2759 13.76106444 00
| Epoch (UTC): | 22 January 2026 04:48:42 |
| Eccentricity: | 0.0039367 |
| inclination: | 82.9378° |
| perigee height: | 949 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 276.7769° |
| argument of perigee: | 258.0712° |
| revolutions per day: | 13.76106444 |
| mean anomaly at epoch: | 216.2759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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