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 00046U 26130.30817022 +.00000000 +00000-0 +67337-4 0 00008
2 00046 66.6885 331.5164 0199826 320.1560 38.5020 14.54834320 08
| Epoch (UTC): | 10 May 2026 07:23:45 |
| Eccentricity: | 0.0199826 |
| inclination: | 66.6885° |
| perigee height: | 568 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 331.5164° |
| argument of perigee: | 320.1560° |
| revolutions per day: | 14.54834320 |
| mean anomaly at epoch: | 38.5020° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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