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 26075.79065346 +.00000000 +00000-0 -10764-3 0 00006
2 23439 64.8133 92.6474 0152936 20.6981 340.0049 11.27583846 07
| Epoch (UTC): | 16 March 2026 18:58:32 |
| Eccentricity: | 0.0152936 |
| inclination: | 64.8133° |
| perigee height: | 1894 km |
| apogee height: | 2151 km |
| right ascension of ascending node: | 92.6474° |
| argument of perigee: | 20.6981° |
| revolutions per day: | 11.27583846 |
| mean anomaly at epoch: | 340.0049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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