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 18429U 26069.63382375 +.00000000 +00000-0 -19091-2 0 00000
2 18429 102.4909 123.2877 0227058 6.3202 147.6183 12.06394299 03
| Epoch (UTC): | 10 March 2026 15:12:42 |
| Eccentricity: | 0.0227058 |
| inclination: | 102.4909° |
| perigee height: | 1470 km |
| apogee height: | 1835 km |
| right ascension of ascending node: | 123.2877° |
| argument of perigee: | 6.3202° |
| revolutions per day: | 12.06394299 |
| mean anomaly at epoch: | 147.6183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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