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 26072.99591619 +.00000000 +00000-0 +31754-4 0 00008
2 27006 99.7686 238.9491 0014187 338.9663 129.0543 13.71092326 05
| Epoch (UTC): | 13 March 2026 23:54:07 |
| Eccentricity: | 0.0014187 |
| inclination: | 99.7686° |
| perigee height: | 985 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 238.9491° |
| argument of perigee: | 338.9663° |
| revolutions per day: | 13.71092326 |
| mean anomaly at epoch: | 129.0543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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