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 26071.91286340 +.00000000 +00000-0 +25459-4 0 00006
2 27006 99.7684 237.8482 0014212 341.8469 183.0783 13.71092252 01
| Epoch (UTC): | 12 March 2026 21:54:31 |
| Eccentricity: | 0.0014212 |
| inclination: | 99.7684° |
| perigee height: | 985 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 237.8482° |
| argument of perigee: | 341.8469° |
| revolutions per day: | 13.71092252 |
| mean anomaly at epoch: | 183.0783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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