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 26065.42572382 +.00000000 +00000-0 +17791-3 0 00005
2 27940 98.3809 240.6851 0012323 324.9476 35.0917 14.69361954 06
| Epoch (UTC): | 06 March 2026 10:13:02 |
| Eccentricity: | 0.0012323 |
| inclination: | 98.3809° |
| perigee height: | 654 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 240.6851° |
| argument of perigee: | 324.9476° |
| revolutions per day: | 14.69361954 |
| mean anomaly at epoch: | 35.0917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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