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 40046U 26106.42070234 +.00000000 +00000-0 +36331-3 0 00003
2 40046 97.7180 273.7422 0036436 210.8737 149.0343 14.98807962 03
| Epoch (UTC): | 16 April 2026 10:05:48 |
| Eccentricity: | 0.0036436 |
| inclination: | 97.7180° |
| perigee height: | 545 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 273.7422° |
| argument of perigee: | 210.8737° |
| revolutions per day: | 14.98807962 |
| mean anomaly at epoch: | 149.0343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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