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 26053.73186705 +.00000000 +00000-0 +69360-3 0 00007
2 40046 97.7084 221.6463 0038069 31.9700 328.3821 14.97968665 09
| Epoch (UTC): | 22 February 2026 17:33:53 |
| Eccentricity: | 0.0038069 |
| inclination: | 97.7084° |
| perigee height: | 547 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 221.6463° |
| argument of perigee: | 31.9700° |
| revolutions per day: | 14.97968665 |
| mean anomaly at epoch: | 328.3821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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