Temperature at Altitude Calculator

Estimate atmospheric temperature with altitude using the standard tropospheric lapse rate.

Altitude temperature estimate
Choose units, enter altitude and a sea-level reference temperature, then apply the ISA lapse rate.

Feet

Degrees Fahrenheit

About temperature at altitude

Air temperature generally decreases with height through the troposphere because rising air expands as atmospheric pressure falls. The International Standard Atmosphere represents this change with a standard lapse rate of 6.5 degrees Celsius per kilometre, or 0.0065 degree per metre. This calculator subtracts that standard decrease from a chosen sea-level reference temperature and reports the result in Celsius, Fahrenheit, and Kelvin. It accepts altitude in metres or feet and a reference temperature in Celsius or Fahrenheit. With the ISA sea-level temperature of 15 degrees Celsius, the model gives 8.5 degrees at 1,000 metres and minus 17.5 degrees at 5,000 metres. The relationship is linear within the lower standard atmosphere: temperature equals base temperature minus lapse rate times altitude in metres. Fahrenheit input is converted to Celsius before the lapse rate is applied, while feet are converted using 0.3048 metre per foot. The final temperature conversions are performed only after the atmospheric calculation. This is a standard-model estimate, not a weather forecast. Actual temperature profiles vary with season, latitude, time of day, air mass, cloud, humidity, and local terrain. Temperature inversions can make air warmer with height, while dry and saturated rising parcels follow different adiabatic lapse rates. Mountain summit temperatures can differ considerably from the value estimated from a distant lowland station. Use current observations and an aviation weather briefing whenever safety or operational decisions depend on atmospheric conditions. The constant 6.5-degree lapse rate is intended for the tropospheric portion of the ISA, extending to about 11 kilometres or 36,000 feet. Above the tropopause, the standard atmosphere uses different layers and the simple linear rule no longer applies. Even below that boundary, a custom measured base temperature improves relevance but does not capture changing lapse rates along the route. The calculator is useful for classroom physics, rough hiking preparation, aviation exercises, meteorology demonstrations, and quick comparisons between elevations. Keep altitude referenced consistently to mean sea level, and distinguish environmental lapse rate from temperature changes experienced by an individual moving air parcel.

Temperature at altitude examples

Examples use a 15 °C sea-level reference and the ISA tropospheric lapse rate.

Altitude and baseEstimated temperatureTemperature decrease
1,000 m; base 15 °CTemperature: 8.5 °C; Temperature: 47.3 °F; Temperature: 281.65 KTemperature decrease: 6.5 °C
5,000 m; base 15 °CTemperature: -17.5 °C; Temperature: 0.5 °F; Temperature: 255.65 KTemperature decrease: 32.5 °C
10,000 ft; base 59 °F-4.81 °C (23.34 °F)19.81 °C below the base

How to estimate temperature at altitude

  1. Enter the altitude and choose whether it is measured in metres or feet.
  2. Enter the sea-level reference temperature and select Celsius or Fahrenheit.
  3. Select Calculate temperature to apply the standard 6.5 °C/km lapse rate.
  4. Treat the result as a standard-atmosphere estimate and compare it with current weather data.

Frequently asked questions

What lapse rate does this calculator use?

It uses the ISA tropospheric lapse rate of 6.5 degrees Celsius per kilometre. That equals 0.0065 degree Celsius per metre.

Is the calculated temperature a weather forecast?

No, it is a standard-atmosphere estimate based on a constant gradient. Real weather can produce different lapse rates and temperature inversions.

Can I enter altitude in feet?

Yes, choose Feet and the calculator converts the value to metres before applying the lapse rate. Results are shown in all three common temperature scales.

Why can mountain temperatures differ from this result?

Humidity, wind, terrain, cloud cover, air masses, and inversions all affect actual temperature. A single constant lapse rate cannot model those local conditions.

Does the formula work above the troposphere?

No, the simple linear rule is intended only through the lower standard atmosphere to roughly 11 kilometres. Higher ISA layers use different temperature gradients.