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 00047U 26037.38501782 +.00000000 +00000-0 +18036-3 0 00007
2 00047 66.6645 38.0994 0225022 235.1266 122.8504 14.45158426 09
| Epoch (UTC): | 06 February 2026 09:14:25 |
| Eccentricity: | 0.0225022 |
| inclination: | 66.6645° |
| perigee height: | 581 km |
| apogee height: | 902 km |
| right ascension of ascending node: | 38.0994° |
| argument of perigee: | 235.1266° |
| revolutions per day: | 14.45158426 |
| mean anomaly at epoch: | 122.8504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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