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 18123U 26146.20887912 +.00000000 +00000-0 +55063-4 0 00007
2 18123 98.7335 332.5721 0011723 220.4647 139.5658 14.19549476 01
| Epoch (UTC): | 26 May 2026 05:00:47 |
| Eccentricity: | 0.0011723 |
| inclination: | 98.7335° |
| perigee height: | 818 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 332.5721° |
| argument of perigee: | 220.4647° |
| revolutions per day: | 14.19549476 |
| mean anomaly at epoch: | 139.5658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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