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 26047.28152243 +.00000000 +00000-0 +10404-3 0 00002
2 00047 66.6657 11.5037 0224293 228.0472 130.1330 14.45170116 04
| Epoch (UTC): | 16 February 2026 06:45:23 |
| Eccentricity: | 0.0224293 |
| inclination: | 66.6657° |
| perigee height: | 582 km |
| apogee height: | 901 km |
| right ascension of ascending node: | 11.5037° |
| argument of perigee: | 228.0472° |
| revolutions per day: | 14.45170116 |
| mean anomaly at epoch: | 130.1330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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