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 27643U 26150.41122439 +.00000000 +00000-0 +48581-3 0 00004
2 27643 94.0241 332.7936 0005879 194.4917 165.6173 15.47517900 09
| Epoch (UTC): | 30 May 2026 09:52:09 |
| Eccentricity: | 0.0005879 |
| inclination: | 94.0241° |
| perigee height: | 420 km |
| apogee height: | 428 km |
| right ascension of ascending node: | 332.7936° |
| argument of perigee: | 194.4917° |
| revolutions per day: | 15.47517900 |
| mean anomaly at epoch: | 165.6173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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