Apollo 7

Apollo 8

Apollo 9

Apollo 10

Apollo 11

Apollo 12

Apollo 13

Apollo 14

Apollo 15

Apollo 16

Apollo 17

CSM/LM at EOI

36,419

87,382

95,231

98,273

100,756.4

101,126.9

101,261.2

102,083.6

107,142

107,226

107,161

CSM/LM at Separation

---

---

---

94,063

96,566.6

---

---

---

---

---

---

CSM/LM at Transposition & Docking

---

---

91,055

94,243

96,767.5

97,119.8

97,219.4

98,037.2

103,105

103,175

103,167

CSM at Transposition & Docking

---

---

58,925

63,560

63,473.0

63,535.6

63,720.3

64,388.0

66,885

66,923

66,893

LM at Transposition & Docking

---

---

32,130

30,683

33,294.5

33,584.2

33,499.1

33,649.2

36,220

36,252

36,274

CSM/LM at 1st MCC Ignition

---

63,307

---

93,889

96,418.2

96,870.6

97,081.5

97,901.5

---

---

---

CSM/LM at 1st MCC Cutoff

---

---

---

93,413

96,204.2

96,401.2

96,851.1

---

---

---

---

CSM/LM Before Cryogenic Tank Anomaly

---

---

---

---

---

---

96,646.9

---

---

---

---

CSM/LM After Cryogenic Tank Anomaly

---

---

---

---

---

---

96,038.7

---

---

---

---

CSM/LM at 2nd MCC Ignition

---

62,845

---

---

---

---

95,959.9

97,104.1

---

---

---

CSM/LM at 2nd MCC Cutoff

---

---

---

---

---

---

95,647.1

---

---

---

---

CSM at TEI Ignition

---

45,931

---

37,254

36,965.7

34,130.6

95,424.0

34,554.4

35,899

38,697

36,394

CSM at TEI Cutoff

---

---

---

26,172

26,792.7

25,724.5

87,456.0

---

---

---

---

CSM at 3rd MCC Ignition

---

32,008

---

---

---

---

87,325.3

24,631.9

---

---

---

CSM at 3rd MCC Cutoff

---

---

---

---

---

---

87,263.3

---

---

---

---

CSM/LM at LOI Ignition

---

62,827

---

93,319

96,061.6

96,261.1

---

97,033.1

102,589

102,642

102,639

CSM/LM at LOI Cutoff

---

46,743

---

69,429

72,037.6

72,335.6

---

71,823.0

76,329

77,647

76,540

CSM/LM at Circularization Ignition

---

46,716

---

69,385

72,019.9

72,243.7

---

---

---

---

---

CSM/LM at Circularization Cutoff

---

---

---

68,455

70,905.9

71,028.4

---

---

---

---

---

CSM/LM at Descent Orbit Insertion

---

---

---

---

---

---

---

71,768.8

76,278

77,595

76,354

CSM/LM at Separation for Lunar Landing

---

---

---

68,238

70,760.3

70,897.3

---

70,162.3

74,460

76,590

74,762

CSM at Separation for Lunar Landing

---

---

---

37,072

37,076.8

36,911.8

---

36,036.4

37,742

39,847

37,991

LM at Separation for Lunar Landing

---

---

---

31,166

33,683.5

33,985.5

---

34,125.9

36,718

36,743

36,771

LM at Powered Descent Initiation

---

---

---

---

---

---

---

34,067.8

36,634

36,617

36,686

LM at Descent Orbit Insertion Ignition

---

---

---

31,137

33,669.6

33,971.8

---

---

---

---

---

LM at Descent Orbit Insertion Cutoff

---

---

---

30,903

33,401.6

33,719.3

---

---

---

---

---

LM at Lunar Landing

---

---

---

---

16,153.2

16,564.2

---

16,371.7

18,175

18,208

18,305

CSM at Plane Burn Time

---

---

---

---

---

---

---

35,610.4

37,219

38,994

37,464

CSM at Circularization Ignition

---

---

---

---

---

---

---

35,996.3

37,716

39,595

37,960

LM at Phasing Ignition

---

---

---

30,824

---

---

---

---

---

---

---

LM at Phasing Cutoff

---

---

---

30,283

---

---

---

---

---

---

---

LM at Fuel Depletion

---

---

5,616

5,243

---

---

---

---

---

---

---

CSM/LM Ascent Stage at Docking

---

---

36,828

44,930

42,585.4

41,071.8

---

39,906.8

41,754

44,318

41,914

CSM at Docking

---

---

26,895

36,995

36,847.4

35,306.2

---

34,125.5

35,928

38,452

36,036

LM Ascent Stage at Lunar Liftoff

---

---

---

---

10,776.6

10,749.6

---

10,779.8

10,915

10,949

10,997

LM Ascent Stage at Orbit Insertion for Docking

---

---

---

8,077

5,928.6

5,965.6

---

5,917.8

5,985

6,001

6,042

LM Ascent Stage at Terminal Phase Initiation

---

---

---

---

---

---

---

5,880.1

5,965

5,972

5,970

LM Ascent Stage After Staging

---

---

---