1000 feet
1500 ft
During IFR flight, ATC will dictate cruising altitude.
it's altitude should be whatever is economical for that flight
We will fly a VFR flight heading 245 - what is a legal cruising altitude?
It can be calculated at any altitude - including negative ones - eg under water.
For IFR (Instrument Flight Rules) flight, the minimum navigation equipment required typically includes a functioning VOR (VHF Omnidirectional Range) receiver, an ADF (Automatic Direction Finder), and either an RNAV (Area Navigation) system or a GPS receiver capable of IFR operations. Additionally, aircraft must be equipped with a transponder with altitude reporting capability, and pilots must have a means to maintain altitude and heading, such as an attitude indicator and a directional gyro. Compliance with specific regulations may vary based on the aircraft type and operational environment.
The minimum altitude of a low Earth orbit is approximately 160 kilometers (100 miles) above the Earth's surface. This altitude allows satellites to remain in orbit while being close enough to the Earth to effectively carry out their functions.
It will vary by country. For example, in the US the minimum visibility is 3 miles.
This question does not provide enough information to be answered.
1,500 feet AGL.
I'm sure that this question means altitude. Altitude is vertical distance between the maximum or minimum of the ocean wave (or any wave) and halfway between the minimum and maximum. Half the vertical distance between the minimum and maximum of the wave.
To measure how high a rocket can go during flight, you can use an altimeter, which measures altitude based on atmospheric pressure or GPS data. Additionally, telemetry systems can send real-time data back to the ground, allowing for precise tracking of the rocket's altitude. After the flight, the maximum altitude can also be determined by analyzing the rocket's flight data logs. Combining these methods provides an accurate assessment of the rocket's peak altitude.