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 27939U 26044.96557458 +.00000000 +00000-0 +31359-3 0 00002
2 27939 98.3409 225.8701 0010415 303.3910 205.4173 14.73185878 04
| Epoch (UTC): | 13 February 2026 23:10:25 |
| Eccentricity: | 0.0010415 |
| inclination: | 98.3409° |
| perigee height: | 644 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 225.8701° |
| argument of perigee: | 303.3910° |
| revolutions per day: | 14.73185878 |
| mean anomaly at epoch: | 205.4173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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