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 23439U 26041.91142662 +.00000000 +00000-0 +16935-3 0 00005
2 23439 64.8160 147.4404 0151686 27.1302 333.7448 11.27583583 09
| Epoch (UTC): | 10 February 2026 21:52:27 |
| Eccentricity: | 0.0151686 |
| inclination: | 64.8160° |
| perigee height: | 1895 km |
| apogee height: | 2150 km |
| right ascension of ascending node: | 147.4404° |
| argument of perigee: | 27.1302° |
| revolutions per day: | 11.27583583 |
| mean anomaly at epoch: | 333.7448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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