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 46702U 26106.10674787 +.00000000 +00000-0 +10079-2 0 00006
2 46702 53.1588 42.9673 0002697 134.5897 225.5326 15.33169122 01
| Epoch (UTC): | 16 April 2026 02:33:43 |
| Eccentricity: | 0.0002697 |
| inclination: | 53.1588° |
| perigee height: | 465 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 42.9673° |
| argument of perigee: | 134.5897° |
| revolutions per day: | 15.33169122 |
| mean anomaly at epoch: | 225.5326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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