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 23318U 26044.66740633 +.00000000 +00000-0 +48212-4 0 00002
2 23318 82.5404 112.6426 0021594 314.2046 45.7392 14.80874673 03
| Epoch (UTC): | 13 February 2026 16:01:03 |
| Eccentricity: | 0.0021594 |
| inclination: | 82.5404° |
| perigee height: | 611 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 112.6426° |
| argument of perigee: | 314.2046° |
| revolutions per day: | 14.80874673 |
| mean anomaly at epoch: | 45.7392° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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