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 23967U 26032.27142663 +.00000000 +00000-0 +00000-0 0 00004
2 23967 10.9845 17.8078 0002705 127.6758 57.3722 1.00251926 09
| Epoch (UTC): | 01 February 2026 06:30:51 |
| Eccentricity: | 0.0002705 |
| inclination: | 10.9845° |
| perigee height: | 35781 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 17.8078° |
| argument of perigee: | 127.6758° |
| revolutions per day: | 1.00251926 |
| mean anomaly at epoch: | 57.3722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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