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 26041.62679184 +.00000000 +00000-0 +50997-4 0 00000
2 23318 82.5409 115.4717 0021839 324.7035 35.2731 14.80872275 05
| Epoch (UTC): | 10 February 2026 15:02:34 |
| Eccentricity: | 0.0021839 |
| inclination: | 82.5409° |
| perigee height: | 611 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 115.4717° |
| argument of perigee: | 324.7035° |
| revolutions per day: | 14.80872275 |
| mean anomaly at epoch: | 35.2731° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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