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 23467U 26140.42822434 +.00000000 +00000-0 +00000-0 0 00007
2 23467 9.7066 13.3246 0003212 36.5560 154.7317 1.00268386 06
| Epoch (UTC): | 20 May 2026 10:16:38 |
| Eccentricity: | 0.0003212 |
| inclination: | 9.7066° |
| perigee height: | 35774 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 13.3246° |
| argument of perigee: | 36.5560° |
| revolutions per day: | 1.00268386 |
| mean anomaly at epoch: | 154.7317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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