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 26017.30887244 +.00000000 +00000-0 +29420-4 0 00001
2 27006 99.7588 182.3693 0015174 118.0004 305.7901 13.71088821 01
| Epoch (UTC): | 17 January 2026 07:24:46 |
| Eccentricity: | 0.0015174 |
| inclination: | 99.7588° |
| perigee height: | 984 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 182.3693° |
| argument of perigee: | 118.0004° |
| revolutions per day: | 13.71088821 |
| mean anomaly at epoch: | 305.7901° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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