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 26073.86553904 +.00000000 +00000-0 +17714-3 0 00004
2 00046 66.6871 125.3749 0195204 2.0142 358.1708 14.54696845 01
| Epoch (UTC): | 14 March 2026 20:46:22 |
| Eccentricity: | 0.0195204 |
| inclination: | 66.6871° |
| perigee height: | 572 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 125.3749° |
| argument of perigee: | 2.0142° |
| revolutions per day: | 14.54696845 |
| mean anomaly at epoch: | 358.1708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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