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 26069.67110875 +.00000000 +00000-0 +75743-4 0 00002
2 23439 64.8134 102.5457 0152702 21.8445 338.8899 11.27583872 06
| Epoch (UTC): | 10 March 2026 16:06:23 |
| Eccentricity: | 0.0152702 |
| inclination: | 64.8134° |
| perigee height: | 1894 km |
| apogee height: | 2151 km |
| right ascension of ascending node: | 102.5457° |
| argument of perigee: | 21.8445° |
| revolutions per day: | 11.27583872 |
| mean anomaly at epoch: | 338.8899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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