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 27432U 26159.18819502 +.00000000 +00000-0 +44191-4 0 00001
2 27432 98.8703 212.0664 0051047 125.2893 304.1771 14.14563013 04
| Epoch (UTC): | 08 June 2026 04:31:00 |
| Eccentricity: | 0.0051047 |
| inclination: | 98.8703° |
| perigee height: | 807 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 212.0664° |
| argument of perigee: | 125.2893° |
| revolutions per day: | 14.14563013 |
| mean anomaly at epoch: | 304.1771° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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