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 26046.17422488 +.00000000 +00000-0 +92680-4 0 00007
2 00047 66.6656 14.4793 0224388 228.8366 129.3194 14.45168527 00
| Epoch (UTC): | 15 February 2026 04:10:53 |
| Eccentricity: | 0.0224388 |
| inclination: | 66.6656° |
| perigee height: | 582 km |
| apogee height: | 901 km |
| right ascension of ascending node: | 14.4793° |
| argument of perigee: | 228.8366° |
| revolutions per day: | 14.45168527 |
| mean anomaly at epoch: | 129.3194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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