Crew vehicle flight deck
A four-seat capsule chasing a space station: orbit display with apoapsis, periapsis and the planned transfer, the 8-ball, RCS quads, the docking camera with range and closure tapes, the burn timer and delta-v budget, a guarded abort-mode switch, caution and warning, ground-station passes and crew biomedical data. All native controls. Try it in Cassette Futurism, Aperture, NERV and Death Star.
Station
Pe 212
Ap 418
Crew
- Apoapsis
- 418.2 km
- Periapsis
- 212.6 km
- Inclination
- 51.64°
- Period
- 90:41
- Phase angle
- +4.2°
- Our orbit
- Station (dashed)
- Planned (dotted)
- Pitch
- −8.0° · −0.1°/s
- Yaw
- +1.2° · 0.0°/s
- Roll
- +14.0° · +0.4°/s
- Error
- 0.3° · deadband 0.5°
- A (firing)
- B
- C (firing)
- D iso (lit)
Y +0.18 mZ −0.11 m
ROLL +0.4°CAPTURE 05:16
Time to ignition
0412
- Δv
- 12.4 m/s
- Burn time
- 0:38
- Attitude
- P 0.0 · Y 180.0 · R 0.0
Delta-v budget, m/s
0
Deorbit 120
After TI
500
Abort executed: back away from the station on +R bar, then deorbit at the next opportunity.
- Cabin press
- Fire
- RCS D iso (lit)
- Fuel cell
- CO₂ high (lit)
- Gimbal lock
- GPS lock (lit)
- Docking tgt (on)
Propellant
FuelReserve1200 kg
OxReserve1920 kg
B1 88%
B2 71%
B3 18%
Oxygen, kPa
CO₂ scrubber load
- Solar arrays
- 2.84 kW · sun
- Bus
- 28.1 V · 61 A
- Cabin
- 101.2 kPa · 22.4 °C
- LOS Hawaii
- AOS relay sat · 22 min
- LOS · 6 min gap
- AOS Wallops
Heart rate trendHeart rateSpO₂
CDR Okafor7298%
PLT Varga9697%
MS Lindqvist6499%