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 26088.16588683 +.00000000 +00000-0 +36550-3 0 00004
2 00046 66.6866 86.3959 0196523 351.2945 8.4771 14.54733248 03
| Epoch (UTC): | 29 March 2026 03:58:52 |
| Eccentricity: | 0.0196523 |
| inclination: | 66.6866° |
| perigee height: | 571 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 86.3959° |
| argument of perigee: | 351.2945° |
| revolutions per day: | 14.54733248 |
| mean anomaly at epoch: | 8.4771° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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