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 23432U 26129.41577115 +.00000000 +00000-0 +82677-4 0 00002
2 23432 74.0297 115.5517 0006663 260.1771 251.8979 14.34453361 00
| Epoch (UTC): | 09 May 2026 09:58:42 |
| Eccentricity: | 0.0006663 |
| inclination: | 74.0297° |
| perigee height: | 772 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 115.5517° |
| argument of perigee: | 260.1771° |
| revolutions per day: | 14.34453361 |
| mean anomaly at epoch: | 251.8979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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