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 26156.82972031 +.00000000 +00000-0 +10609-3 0 00005
2 00047 66.6651 77.0994 0214308 147.9317 213.5040 14.45296106 02
| Epoch (UTC): | 05 June 2026 19:54:47 |
| Eccentricity: | 0.0214308 |
| inclination: | 66.6651° |
| perigee height: | 588 km |
| apogee height: | 894 km |
| right ascension of ascending node: | 77.0994° |
| argument of perigee: | 147.9317° |
| revolutions per day: | 14.45296106 |
| mean anomaly at epoch: | 213.5040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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