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 26129.96444058 +.00000000 +00000-0 +69918-4 0 00000
2 00046 66.6885 332.4535 0199811 320.4079 38.2578 14.54834074 03
| Epoch (UTC): | 09 May 2026 23:08:47 |
| Eccentricity: | 0.0199811 |
| inclination: | 66.6885° |
| perigee height: | 568 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 332.4535° |
| argument of perigee: | 320.4079° |
| revolutions per day: | 14.54834074 |
| mean anomaly at epoch: | 38.2578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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