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 26065.39088810 +.00000000 +00000-0 +26872-4 0 00003
2 27006 99.7671 231.2191 0014442 358.7826 30.8588 13.71092061 01
| Epoch (UTC): | 06 March 2026 09:22:52 |
| Eccentricity: | 0.0014442 |
| inclination: | 99.7671° |
| perigee height: | 985 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 231.2191° |
| argument of perigee: | 358.7826° |
| revolutions per day: | 13.71092061 |
| mean anomaly at epoch: | 30.8588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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