Event

GET

(hhh:mm:ss)

Altitude

(n mi)

Space

Fixed

Velocity

(ft/sec)

Event

Duration

(sec)

Velocity

Change

(ft/sec)

Apolune

(n mi)

Perilune

(n mi)

Lunar orbit insertion ignition

081:56:40.70

87.4

8,061.4

Lunar orbit insertion cutoff

082:02:51.54

64.2

5,458.5

370.84

3,022.4

169.0

58.1

Descent orbit insertion ignition

086:10:52.97

59.2

5,484.8

Descent orbit insertion cutoff

086:11:13.78

59

5,279.5

20.81

205.7

58.8

9.1

CSM/LM undocking/separation ignition

103:47:41.6

30.5

5,435.8

CSM/LM undocking/separation cutoff

103:47:44.3

2.7

0.8

60.2

7.8

CSM orbit circularization ignition

105:11:46.11

60.5

5,271.3

CSM orbit circularization cutoff

105:11:50.13

60.3

5,342.1

4.02

77.2

63.9

56.0

LM powered descent initiation

108:02:26.52

7.8

5,565.6

LM powered descent cutoff

108:15:11.13

764.61

CSM plane change ignition

117:29:33.17

62.1

5,333.1

CSM plane change cutoff

117:29:51.67

62.1

5,333.3

18.50

370.5

62.1

57.7

LM lunar liftoff ignition

141:45:40

Lunar ascent orbit cutoff

141:52:52.1

432.1

6,066.1

51.7

8.5

LM vernier adjustment ignition

141:56:49.4

11.1

5,548.5

LM vernier adjustment cutoff

141:57:01.5

12.1

10.3

51.2

8.4

LM terminal phase initiation ignition

142:30:51.1

44.8

5,396.6

LM terminal phase initiation cutoff

142:30:54.7

3.6

88.5

60.1

46.0

LM terminal phase finalize ignition

143:13:29.1

58.8

5,365.5

LM terminal phase finalize cutoff

143:13:55.8

26.7

32

61.5

58.2

CSM/LM docked

143:32:50.5

58.6

5,353.5

LM ascent stage jettisoned

145:44:58.0

59.9

5,344.6

CSM/LM final separation ignition

145:49:42.5

60.6

5,341.7

CSM/LM final separation cutoff

145:49:58.3

15.8

3.4

63.4

56.8

LM ascent stage deorbit ignition

147:14:16.9

57.2

5,358.7

LM ascent stage fuel depletion

147:15:33.1

57.2

5,177

76.2

186.1

56.7

-59.8