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 27431U 26104.15117461 +.00000000 +00000-0 +50396-4 0 00006
2 27431 98.9586 154.7543 0016296 65.1821 295.1042 14.10215936 05
| Epoch (UTC): | 14 April 2026 03:37:41 |
| Eccentricity: | 0.0016296 |
| inclination: | 98.9586° |
| perigee height: | 847 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 154.7543° |
| argument of perigee: | 65.1821° |
| revolutions per day: | 14.10215936 |
| mean anomaly at epoch: | 295.1042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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