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 27940U 26162.25573988 +.00000000 +00000-0 +80481-4 0 00004
2 27940 98.3873 340.0748 0013428 21.2290 338.9469 14.69483074 00
| Epoch (UTC): | 11 June 2026 06:08:15 |
| Eccentricity: | 0.0013428 |
| inclination: | 98.3873° |
| perigee height: | 653 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 340.0748° |
| argument of perigee: | 21.2290° |
| revolutions per day: | 14.69483074 |
| mean anomaly at epoch: | 338.9469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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