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 26145.40338722 +.00000000 +00000-0 +52329-3 0 00008
2 40046 97.7184 312.3432 0039115 84.9108 275.6578 14.99246920 05
| Epoch (UTC): | 25 May 2026 09:40:52 |
| Eccentricity: | 0.0039115 |
| inclination: | 97.7184° |
| perigee height: | 542 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 312.3432° |
| argument of perigee: | 84.9108° |
| revolutions per day: | 14.99246920 |
| mean anomaly at epoch: | 275.6578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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