As of right now, this is a partial solution
I set up a solution using a non-linear, non-separable first order differential equation. I ran out of brainpower midway through this post, and can't solve that right now, but I will revisit it later. If someone else can solve first, please edit this post. I wanted to post what I had, in case anyone can find errors now, and to re-type my notes more legibly.
Principles
Assume that heated air rises at the sub-stellar point and proceeds at high altitude equivalent to Earth's stratosphere towards the poles, where it enters the 'dark side', a cool, infinite heat sink and heat source. Cool air from the 'dark side' returns in the surface layer equivalent to our troposphere. It moves towards the sub-stellar spot, heating up along the way as it absorbs solar radiation.
We will calculate the energy balance of this surface layer of the atmosphere to calculate a delta-T as a function of angular distance from the sub-stellar spot. The angular distance where delta-T = -25 is the answer to the question.
Data and simplifying assumptions
Data on radiation and atmopsheric circulation taken from here. This reference will be referred to as Fig. X of data.
No land-sea interface; that is, the planet is either all land or all ocean. No heat transport from ocean circulation.
Insolation at the sub-stellar point is equivalent to earth's equator.
Heated air rises at sub-stellar and travels towards the dark side in the upper atmosphere. Cold air returns from the dark side in the lower atmosphere.
The 'dark side' is an infinite, constant low temperature heat source for returning winds.
Ignore effects of expansion and contraction of air when approaching and departing sub-stellar point.
We will calculate atmospheric delta Ts from radiation balance in two bands, an upper atmosphere band, and lower atmosphere band.
Atmosphere is mass $5.15\times10^{18}\text{kg}$, surface area of earth is $5.10\times10^{14} \text{m}^2$ for air column mass of $1.01\times10^{4} \frac{\text{kg}}{\text{m}^2}$.
Lower layer is equivalent to troposphere, everything from sea level to 10 miles, with 75% of the atmosphere's mass, with air column density 7.5 $\frac{\text{kg}}{\text{m}^2}$, Upper layer is rest of atmosphere, air column density 2.5 $\frac{\text{kg}}{\text{m}^2}$.
From figure 1.3 of data, 0.67 of energy absorption is from surface, 0.33 by atmosphere, of which 0.25 is lower layer (by above definition) and 0.08 by upper layer. We will simplify that all absorption is in lower layer.
Assume solar energy absorption and radiation to space are the dominant means of energy transfer. Ignore heat transfer between upper and lower layers.
Assume isometric heating and cooling, specific heat of air is constant 718 $\frac{\text{J}}{\text{kg}\cdot\text{K}}$.
Calculating Energy Balance for the Lower Atmosphere
Simplifying Fig 1.7 of data, Incoming radiation is 300 W/m^2*month at the 0 from substellar, 0 at 90 from substellar, and linear in between.
Temperature change due to energy input is: $$E_{in} = \frac{300 - \frac{10}{3}\gamma\,\frac{\text{W}}{\text{m}^2}}{7.5\frac{\text{kg}}{\text{m}^2}\cdot718\frac{\text{J}}{\text{kg}\cdot\text{K}}} = 0.0557 - 0.000619\gamma\, \frac{\text{K}}{\text{s}}\quad\quad 0^\circ < \gamma < 90^\circ$$ where $\gamma$ is the angle from the sub-stellar point
Simplifying Fig 1.7 of data, Outgoing radiation is 250 W/m^2*month at 0 from substellar, since temperatures are similar to earth's at the equator. By Stefan Boltzmann law, radiative heat transfer is proportional to the fourth power of Temperature. Temperatures must be calculated in Kelvin.
Temperature change due to energy output is: $$E_{out} = \frac{250 \left(\frac{\text{T}}{298}\right)^4\,\frac{\text{W}}{\text{m}^2}}{7.5\frac{\text{kg}}{\text{m}^2}\cdot718\frac{\text{J}}{\text{kg}\cdot\text{K}}} = 5.9\times10^{-12}T^4 \, \frac{\text{K}}{\text{s}}$$
where $T$ is temperature in Kelvin.
Wind Speed and Pressure assumptions
Changes in temperature drive changes in pressure which drive changes in wind speed which drive the temperature gradient. To avoid solving three simultaneous differential equations, ignore the effect of pressure changes on wind speed.
We will model the expected strong, constant winds at 10 m/s and 20 m/s.
A degree of latitude is 111 km. The ratio between distance and angle is $9.0\times10^{-6}\frac{\text{degrees}}{\text{m}}$. A translation of the above wind speeds to angular velocities is $9.0\times10^{-5}\frac{\text{degrees}}{\text{s}}$ and $1.8\times10^{-4}\frac{\text{degrees}}{\text{s}}$.
Differential Equation and Solution(?)
Overall energy balance for the atmopspheric circulation is, after converting angle to time using the 10 m/s wind speed:
$$\frac{dT}{dt} = 0.0557 - 5.6\times10^{-8}t - 5.9\times10^{-12}T^4$$.
EDIT:
After attempting to solve numerically using an Euler method, I discovered that this does not work. My problem is ignoring the potential energy imparted to air molecules to raise them from the lower atmosphere to the upper atmosphere. This takes something like 5e8 W at the 10 m/s flow I calculated and needs to be accounted for. Still working.