Table 4
Differences in 
and amplitudes of the periodic variations caused by the mass-dependent errors between LTE430 and LTE440.
| Contributing body i |  |
 |
Ai[s] | ∣∆ Mi / Mi ∣× Ai [s] |
|---|---|---|---|---|
| Sun | 1.5 × 10−8 | 7.4 × 10−20 | 1.6 × 10−3 | 7.9 × 10−15 |
| Mercury | 1.7 × 10−15 | −6.8 × 10−21 | 1.9 × 10−9 | 7.6 × 10−15 |
| Venus | 2.9 × 10−14 | 4.1 × 10−30 | 2.0 × 10−7 | 2.8 × 10−23 |
| Earth | 1.2 × 10−11 | 1.5 × 10−21 | 2.9 × 10−7 | 3.7 × 10−17 |
| Mars System | 2.4 × 10−15 | −3.3 × 10−23 | 5.0 × 10−8 | 7.0 × 10−16 |
| Jupiter System | 1.8 × 10−12 | 9.9 × 10−21 | 7.5 × 10−6 | 4.1 × 10−14 |
| Saturn System | 3.0 × 10−13 | 2.8 × 10−21 | 2.5 × 10−6 | 2.4 × 10−14 |
| Uranus System | 2.2 × 10−14 | −3.0 × 10−20 | 4.5 × 10−7 | 6.0 × 10−13 |
| Neptune System | 1.7 × 10−14 | −9.3 × 10−28 | 1.2 × 10−7 | 6.6 × 10−21 |
| Pluto System | 1.8 × 10−18 | 2.8 × 10−21 | 5.8 × 10−10 | 8.9 × 10−13 |
| Total | 1.5 × 10−8 | 5.4 × 10−20 | – | – |
Notes. 
is derived from Table 2, and Ai is estimated from the periodic variation of each contributing body in LTE440. The 
and Ai of the Sun are assumed to be the sum of the contribution by the square of lunar velocity and the gravitational potential of the Sun at the Moon. ∆Mi/Mi denotes the relative mass difference of body i between DE430 and DE440.
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