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 40332U 26145.59464847 +.00000000 +00000-0 +00000-0 0 00000
2 40332 0.0380 110.1522 0007720 328.3103 73.8744 1.00270840 08
| Epoch (UTC): | 25 May 2026 14:16:17 |
| Eccentricity: | 0.0007720 |
| inclination: | 0.0380° |
| perigee height: | 35754 km |
| apogee height: | 35819 km |
| right ascension of ascending node: | 110.1522° |
| argument of perigee: | 328.3103° |
| revolutions per day: | 1.00270840 |
| mean anomaly at epoch: | 73.8744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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