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 18232U 26073.82618642 +.00000000 +00000-0 +17550-1 0 00003
2 18232 102.9135 276.2293 0207376 212.8324 163.7417 13.98953017 02
| Epoch (UTC): | 14 March 2026 19:49:42 |
| Eccentricity: | 0.0207376 |
| inclination: | 102.9135° |
| perigee height: | 747 km |
| apogee height: | 1048 km |
| right ascension of ascending node: | 276.2293° |
| argument of perigee: | 212.8324° |
| revolutions per day: | 13.98953017 |
| mean anomaly at epoch: | 163.7417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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