Convert Orbital Speed (ISS) to Mach 1
Convert Orbital Speed (ISS) (v_orb) to Mach 1 (Ma) instantly and accurately.
Conversion Formula
Ma = v_orb × 22.51021188
About Orbital Speed (ISS)
The ISS orbits at ~408 km altitude at ≈7,660 m/s (27,576 km/h) - the practical LEO benchmark. At this speed it completes one orbit in 92.68 min (15.5 orbits per day), giving astronauts 16 sunrises and sunsets every 24 hours. Delta-v to reach LEO from Earth's surface is ~9,400 m/s (with gravity and drag losses). GEO at 35,786 km requires only ~3,075 m/s per Kepler's third law. 1 ISS speed ≈ 7,660 m/s.
About Mach 1
Mach 1 = the speed of sound in dry air at ISA sea-level (15°C, 101.325 kPa) = exactly 340.29 m/s (1,225 km/h; 761 mph). Chuck Yeager first exceeded it on 14 October 1947 in the Bell X-1. At 35,000 ft cruise altitude (−56.5°C), it falls to 295.1 m/s. Flight regimes: subsonic
Quick Reference Table
| Orbital Speed (ISS) (v_orb) | Mach 1 (Ma) |
|---|---|
| 1 v_orb | 22.5102 Ma |
| 2 v_orb | 45.0204 Ma |
| 5 v_orb | 112.551 Ma |
| 10 v_orb | 225.102 Ma |
| 25 v_orb | 562.755 Ma |
| 50 v_orb | 1125.51 Ma |
| 100 v_orb | 2251.02 Ma |