Free Temperature at Altitude Calculator
Based on the ISA (International Standard Atmosphere) model. Valid for altitudes from sea level up to 86 km.
Enter sea-level temperature and altitude
Understanding How Atmospheric Temperature Changes with Altitude
The Temperature at Altitude Calculator (also referred to as an ISA Temperature Calculator) is a free online tool that provides quick approximations of the atmospheric temperature at any altitude up to 90 km. Whether you are curious about the temperature at commercial cruising altitudes or need accurate data for flight planning and meteorology, this tool simplifies the process using the International Standard Atmosphere (ISA) model.
Why Temperature Doesn’t Always Drop with Height
A widespread belief is that temperature falls steadily the higher you go. In reality, Earth’s atmosphere is composed of several layers, each with its own thermal behavior. The ISA model accounts for these variations and uses geopotential altitude rather than simple geometric height. Geopotential altitude corrects for gravitational differences caused by latitude, longitude, and elevation, offering a more consistent reference for atmospheric properties. For most lower-altitude applications, the difference between the two height measures is negligible, so you can enter your ordinary altitude directly.
Temperature vs. Altitude: Layer‑by‑Layer Breakdown
The ISA model divides the atmosphere up to 86 km (approximately 53 mi) into distinct zones. The table below summarizes the temperature trend and lapse rate for each layer.
| Layer | Altitude Range | Temperature Trend | Typical Lapse Rate |
|---|---|---|---|
| Troposphere | 0 – 12 km (0 – 7 mi) | Decreases with height | –6.5 °C/km (–18.8 °F/mi; –3.56 °F/1000 ft) |
| Tropopause | Top of troposphere (~12 km) | Constant | –55 °C (–67 °F) |
| Stratosphere | 12 – 51 km (7 – 32 mi) | Increases with height | +1 to +2.8 °C/km (+2.9 to +8.1 °F/mi) |
| Stratopause | 48 – 51 km | Constant | ≈ –1 °C (≈ 30 °F) |
| Mesosphere | 51 – 86 km (32 – 53 mi) | Decreases with height | –2 to –2.8 °C/km (–5.8 to –8.1 °F/mi) |
| Mesopause | ~86 km | Constant | ≈ –87 °C (–124.6 °F); can drop to –100 °C (–148 °F) |
Troposphere
The troposphere is heated directly by Earth’s surface. As you move away from that heat source, the air becomes colder. The standard lapse rate here is 6.5 °C per kilometer (or 3.56 °F per 1000 ft).
Stratosphere
The stratosphere contains the ozone layer, which absorbs most of the Sun’s ultraviolet radiation. This absorption heats the air, so temperature increases with altitude. The warming rate varies between about 1 °C/km and 2.8 °C/km (2.9 to 8.1 °F/mi).
Mesosphere
Above the stratosphere, the mesosphere sees a renewed cooling trend. The temperature drops by 2 to 2.8 °C/km (5.8 to 8.1 °F/mi), reaching the lowest values in Earth’s atmosphere at the mesopause.
Practical Example: Temperature at 35,000 Feet
Suppose you are at an elevation of 2,640 ft with a current temperature of 59 °F, and you want to know the temperature at a typical cruising altitude of 35,000 ft. Because 35,000 ft lies in the troposphere, you use the tropospheric lapse rate.
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Find the altitude difference:
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Multiply by the lapse rate (in °F per foot):
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Subtract this change from the starting temperature because temperature decreases with height:
Thus, at 35,000 ft the expected temperature is approximately –56.2 °F (about –49 °C). The same logic applies in metric units: for every kilometer climbed, subtract 6.5 °C.
The Altitude Temperature Calculator handles all these steps automatically. You simply provide your current altitude and temperature (or sea‑level conditions) and the target height; the tool applies the correct ISA lapse rate for the relevant atmospheric layer and returns the result instantly.
Summary
- Temperature does not always decrease with altitude; the direction and rate of change depend on the atmospheric layer.
- The ISA model, using geopotential altitude, provides a standard reference for predicting temperature at altitude.
- The calculator covers altitudes from 0 to 90 km, encompassing the troposphere, stratosphere, and mesosphere.
- Whether you need the atmospheric temperature at altitude for aviation, meteorology, or general curiosity, this tool delivers reliable estimates.
FAQ
1. How does the Temperature at Altitude Calculator determine the temperature at a given height?
The calculator uses the International Standard Atmosphere (ISA) model, applying the appropriate lapse rate for each atmospheric layer (e.g., –6.5 °C/km in the troposphere, +1 to 2.8 °C/km in the stratosphere). You provide a reference temperature and altitude, and the tool computes the temperature at your target altitude.
2. Why does the stratosphere get warmer with increasing altitude?
The stratosphere contains the ozone layer, which absorbs most of the Sun's ultraviolet radiation. This absorption converts UV energy into heat, causing temperature to rise as you go higher in this layer.
3. What is the difference between geopotential altitude and geometric altitude?
Geometric altitude is the actual distance above sea level. Geopotential altitude adjusts for variations in gravity (due to latitude, longitude, and elevation) to provide a more consistent measure for atmospheric modeling. The ISA model uses geopotential altitude, though for lower altitudes the difference is small.
4. What typical temperature can be expected at a cruising altitude of 35,000 ft?
At 35,000 ft (about 10.7 km), which lies in the troposphere, the temperature is typically around –56 °F (–49 °C) when the sea‑level temperature is 59 °F. The exact value depends on your starting temperature and altitude.
How to Use
- Enter the temperature at sea level and select the unit (Celsius, Fahrenheit, or Kelvin).
- Enter the altitude and select the unit (meters, kilometers, feet, yards, or miles).
- The calculator instantly shows the temperature at your chosen altitude using the ISA model.