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 26104.25314502 +.00000000 +00000-0 +16305-3 0 00006
2 00046 66.6893 42.5435 0197858 339.3483 19.9708 14.54793602 09
| Epoch (UTC): | 14 April 2026 06:04:31 |
| Eccentricity: | 0.0197858 |
| inclination: | 66.6893° |
| perigee height: | 570 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 42.5435° |
| argument of perigee: | 339.3483° |
| revolutions per day: | 14.54793602 |
| mean anomaly at epoch: | 19.9708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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