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 26139.92148465 +.00000000 +00000-0 +52117-4 0 00005
2 27940 98.3866 317.1460 0014328 86.7986 273.4858 14.69456236 01
| Epoch (UTC): | 19 May 2026 22:06:56 |
| Eccentricity: | 0.0014328 |
| inclination: | 98.3866° |
| perigee height: | 653 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 317.1460° |
| argument of perigee: | 86.7986° |
| revolutions per day: | 14.69456236 |
| mean anomaly at epoch: | 273.4858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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