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 27006U 26039.49366383 +.00000000 +00000-0 +41477-4 0 00007
2 27006 99.7625 204.9039 0015196 63.9331 5.3307 13.71090635 02
| Epoch (UTC): | 08 February 2026 11:50:52 |
| Eccentricity: | 0.0015196 |
| inclination: | 99.7625° |
| perigee height: | 984 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 204.9039° |
| argument of perigee: | 63.9331° |
| revolutions per day: | 13.71090635 |
| mean anomaly at epoch: | 5.3307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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