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 26162.47774670 +.00000000 +00000-0 +56203-4 0 00006
2 23432 74.0327 54.9951 0005771 199.6962 337.3948 14.34463446 00
| Epoch (UTC): | 11 June 2026 11:27:57 |
| Eccentricity: | 0.0005771 |
| inclination: | 74.0327° |
| perigee height: | 773 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 54.9951° |
| argument of perigee: | 199.6962° |
| revolutions per day: | 14.34463446 |
| mean anomaly at epoch: | 337.3948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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