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 26037.70777150 +.00000000 +00000-0 +69155-4 0 00002
2 23318 82.5414 119.1177 0022152 338.0028 22.0232 14.80869040 07
| Epoch (UTC): | 06 February 2026 16:59:11 |
| Eccentricity: | 0.0022152 |
| inclination: | 82.5414° |
| perigee height: | 611 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 119.1177° |
| argument of perigee: | 338.0028° |
| revolutions per day: | 14.80869040 |
| mean anomaly at epoch: | 22.0232° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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