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 26037.43731329 +.00000000 +00000-0 +17972-3 0 00004
2 27940 98.3768 211.9765 0013932 52.2878 307.9588 14.69314762 09
| Epoch (UTC): | 06 February 2026 10:29:43 |
| Eccentricity: | 0.0013932 |
| inclination: | 98.3768° |
| perigee height: | 653 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 211.9765° |
| argument of perigee: | 52.2878° |
| revolutions per day: | 14.69314762 |
| mean anomaly at epoch: | 307.9588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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