Cislunar Space Beginner's GuideCislunar Space Beginner's Guide
Satellite Orbit Simulation
Cislunar Glossary
Resources & Tools
Blue Team Research
Space News
AI Q&A
Forum
Home
Gitee
GitHub
  • 简体中文
  • English
Satellite Orbit Simulation
Cislunar Glossary
Resources & Tools
Blue Team Research
Space News
AI Q&A
Forum
Home
Gitee
GitHub
  • 简体中文
  • English
  • Site map

    • Home (overview)
    • Intro · what is cislunar space
    • Orbits · spacecraft trajectories
    • Frontiers · directions & labs
    • Glossary · terms & definitions
    • Tools · data & code
    • News · space industry archive
    • Topic · blue-team research
  • Cislunar glossary (terms & definitions)

    • Cislunar Space Glossary
    • Dynamics models

      • Circular Restricted Three-Body Problem (CR3BP)
      • CR3BP with Low-Thrust (CR3BP-LT)
      • A2PPO (Attention-Augmented Proximal Policy Optimization)
      • Curriculum Learning
      • Low-Thrust Transfer MDP Formulation
      • Generalized Advantage Estimation (GAE)
      • Direct Collocation
      • Birkhoff-Gustavson Normal Form
      • Central Manifold
      • Action-Angle Variables
      • Poincaré Section
      • Clohessy-Wiltshire (CW) Equation
      • Patched Method (拼接法)
      • Continuation (延拓)
      • Differential Correction (微分修正)
      • Poincaré Map (庞加莱图)
      • Impulsive Maneuver (脉冲机动)
      • Zero-Velocity Surface
      • Hill Three-Body Problem
      • Bicircular Four-Body Problem
      • Quasi-Bicircular Four-Body Problem
      • Strobe Map
      • Stability Set
      • Backward Stability Set
      • Capture Set
      • /en/glossary/dynamics/batch-deployment.html
      • /en/glossary/dynamics/state-dependent-tsp.html
      • /en/glossary/dynamics/q-law.html
      • /en/glossary/dynamics/mass-discontinuity.html
      • /en/glossary/dynamics/equinoctial-elements.html
      • /en/glossary/dynamics/dynamic-programming.html
      • /en/glossary/dynamics/coasting-arc.html
    • Mission orbits

      • Distant Retrograde Orbit (DRO)
      • Near-Rectilinear Halo Orbit (NRHO)
      • Earth-Moon L1/L2 Halo Orbit (EML1/EML2 Halo)
      • DRO Constellation
      • Orbit Identification
      • Transfer Orbit (转移轨道)
      • Perilune (近月点)
      • Apolune (远月点)
      • Retrograde (逆行)
      • Prograde (顺行)
      • Parking Orbit (停泊轨道)
      • Free-Return Trajectory (自由返回轨道)
      • Halo Orbit (Halo 轨道)
      • Lissajous Orbit (Lissajous 轨道)
      • Lyapunov Orbit (Lyapunov 轨道)
      • Cycler Trajectory
      • Multi-Revolution Halo Orbit
      • Ballistic Capture Orbit
      • Low-Energy Transfer Orbit
      • Full Lunar Surface Coverage Orbit
      • /en/glossary/orbits/hub-and-spoke.html
    • Navigation

      • X-ray Pulsar Navigation
      • LiAISON Navigation
    • Lunar minerals

      • Changeite-Mg (Magnesium Changeite)
      • Changeite-Ce (Cerium Changeite)
    • Other

      • Starshade
      • Noncooperative Target
      • Spacecraft Intention Recognition
      • Chain-of-Thought (CoT) Prompting
      • Low-Rank Adaptation (LoRA)
      • Prompt Tuning (P-tuning)
      • Cislunar Space (地月空间)
      • Low Earth Orbit / LEO (低地球轨道)
      • Lunar Gravity Assist / LGA (月球借力)
      • Powered Lunar Flyby / PLF (有动力月球借力)
      • Weak Stability Boundary / WSB (弱稳定边界)
      • /en/glossary/other/libration-point.html
      • Orbit Insertion (入轨)
      • /en/glossary/other/orbital-residence-platform.html
    • Organizations

      • Anduril Industries
      • Booz Allen Hamilton
      • General Dynamics Mission Systems
      • GITAI USA
      • Lockheed Martin
      • Northrop Grumman
      • Quindar
      • Raytheon Missiles & Defense
      • Sci-Tec
      • SpaceX
      • True Anomaly
      • Turion Space
    • Military space doctrine

      • Space Superiority
      • Competitive Endurance
      • DOTMLPF-P Framework
      • Mission Command
      • Force Design
      • Force Development
      • Force Generation
      • Force Employment
      • Space Force Generation Process (SPAFORGEN)
      • Mission Delta (MD)
      • System Delta (SYD)
      • Space Mission Task Force (SMTF)
      • Commander, Space Forces (COMSPACEFOR)
      • Component Field Commands
      • Space Domain Awareness (SDA)
      • Counterspace Operations
      • Resilient/Disaggregated Architecture
      • Operational Test and Training Infrastructure (OTTI)
      • Golden Dome
    • Observation techniques

      • Image Stacking
      • Shift-and-Add (SAA)
      • Synthetic Tracking
      • Sidereal Tracking
      • Signal-to-Noise Ratio (SNR)
      • Astrometry
      • Source Extraction
      • Ephemeris Correlation
      • Cislunar Moving Objects
      • Lunar Glare Zone
      • Image Registration
      • Background Star Elimination
      • Segmentation Map
      • Hot Pixel
    • Satellite Communication & TT&C

      • BeiDou Satellite System
      • Inter-Satellite Link (ISL)
      • All-Time Seamless Communication
      • Constellation Networking
      • Microwave Link
      • Laser-Microwave Communication

Prograde

Author: CislunarSpace

Website: https://cislunarspace.cn

Definition

Prograde refers to the motion state where a spacecraft's direction of travel is the same as the central body's rotation or orbital direction. In the Earth-Moon rotating reference frame, a prograde orbit appears as counterclockwise motion around the Moon. The opposite is retrograde orbit, where the motion direction is opposite to the central body's motion.

Key Elements

Meaning of Prograde in the Earth-Moon System

In the Earth-Moon rotating reference frame, the definitions of prograde and retrograde are based on the Moon's orbital direction around Earth:

  • Prograde orbit: The spacecraft's motion around the Moon is in the same direction as the Moon's orbit around Earth, appearing as counterclockwise motion in the rotating frame
  • Retrograde orbit: The spacecraft's motion around the Moon is opposite to the Moon's orbit around Earth, appearing as clockwise motion in the rotating frame

Most natural celestial bodies (such as the Moon orbiting Earth, Earth orbiting the Sun) move in prograde, making prograde orbits the "conventional" motion state in a sense.

Characteristics of Prograde Orbits in DRO Transfer

Research by Wei et al. (2026) shows that during transfers from LEO to DRO, prograde orbits typically have higher impulsive consumption than retrograde orbits. Reasons for this difference include:

  • Coriolis force direction: In the rotating frame, the Coriolis force for prograde motion aligns with the direction of travel, producing an "acceleration" effect that makes it harder for the spacecraft to be captured into the target orbit during gravity assist
  • Asymmetric energy channels: In the Earth-Moon rotating frame, the energy channel structures in prograde and retrograde directions are asymmetric; the prograde direction typically requires more energy injection
  • Gravity assist efficiency: Lunar gravity assist in the prograde direction usually produces less orbital energy change than in the retrograde direction

Relationship Between Prograde and DRO

DRO (Distant Retrograde Orbit) is inherently a retrograde orbit. If one attempts to design prograde periodic orbits around the Moon, the following categories are typically considered:

  • Prograde near-lunar orbits: Prograde orbits close to the Moon, with significant non-spherical gravitational perturbation
  • Lissajous/Halo orbits: The motion direction of orbits around libration points has special characteristics in the synodic frame
  • Prograde DRO-like orbits: Theoretically exist, but their stability and impulsive consumption are inferior to retrograde DRO

Velocity Vector Description

The angular momentum direction of prograde motion aligns with the zzz-axis of the rotating frame:

hz=(r×v)⋅z^>0h_z = (\mathbf{r} \times \mathbf{v}) \cdot \hat{\mathbf{z}} > 0 hz​=(r×v)⋅z^>0

In the inertial frame, prograde means the spacecraft's velocity component in the equatorial or orbital plane aligns with the central body's rotation direction. In the synodic frame, this relationship additionally accounts for the frame's rotational angular velocity.

Application Value

Prograde motion characteristics have fundamental significance in orbital mechanics:

  • Orbital classification basis: Prograde and retrograde are basic classifications for describing orbital motion direction, serving as prerequisites for understanding special orbits like DRO
  • Transfer scheme comparison: In DRO transfer design, prograde schemes serve as baselines against retrograde schemes, helping analyze the physical roots of impulsive consumption differences
  • Natural orbit reference: Most natural satellites and planets have prograde orbits; prograde orbit theory provides the foundation for understanding solar system body motion
  • Orbit-keeping strategies: Prograde and retrograde orbit maintenance strategies differ; the different Coriolis force directions directly affect orbit control strategy design

Related Concepts

  • Retrograde
  • Distant Retrograde Orbit (DRO)

References

  • Wei Z et al. Research on lunar gravity-assist injection into cislunar distant retrograde orbit families[J]. 2026.
  • Vallado D A. Fundamentals of Astrodynamics and Applications[M]. 4th ed. 2013.
  • Whitley R, Martinez R. Options for staging orbits in cislunar space[C]. 2016.
Improve this page
Last Updated: 4/29/26, 11:30 AM
Contributors: Cron Job
Prev
Retrograde (逆行)
Next
Parking Orbit (停泊轨道)
地月空间入门指南
Cislunar Space Beginner's GuideYour guide to cislunar space
View on GitHub

Navigate

  • Home
  • About
  • Space News
  • Glossary

Content

  • Cislunar Orbits
  • Research
  • Resources
  • Blue Team

English

  • Home
  • About
  • Space News
  • Glossary

Follow Us

© 2026 Cislunar Space Beginner's Guide  |  湘ICP备2026006405号-1
Related:智慧学习助手 UStudy航天任务工具箱 ATK
支持我
鼓励和赞赏我感谢您的支持