Apollo 16 Lunar Orbit Phase
Event |
GET (hhh:mm:ss) |
Altitude (n mi) |
Space Fixed Velocity (ft/sec) |
Event Duration (sec) |
Velocity Change (ft/sec) |
Geodetic Latitude (deg N) |
Longitude (deg E) |
Apolune (n mi) |
Perilune (n mi) |
Lunar orbit insertion ignition |
074:28:27.87 |
93.9 |
8,105.4 |
|
|
8.15 |
-166.63 |
|
|
Lunar orbit insertion cutoff |
074:34:42.77 |
75.3 |
5,399.2 |
374.90 |
2,802 |
7.12 |
169.32 |
170.3 |
58.1 |
Descent orbit insertion ignition |
078:33:45.04 |
58.5 |
5,486.3 |
|
|
8.58 |
136.02 |
|
|
Descent orbit insertion cutoff |
078:34:09.39 |
58.4 |
5,281.9 |
24.35 |
209.5 |
8.58 |
-137.27 |
58.5 |
10.9 |
LM undocking and separation |
096:13:31 |
33.8 |
5,417.2 |
|
|
2.37 |
121.92 |
|
|
CSM orbit circularization ignition |
103:21:43.08 |
59.2 |
5,277.8 |
|
|
9.22 |
-151.98 |
|
|
CSM orbit circularization cutoff |
103:21:47.74 |
59.1 |
5,348.7 |
4.66 |
81.6 |
9.23 |
-151.95 |
68.0 |
53.1 |
LM powered descent initiation |
104:17:25 |
10.944 |
5,548.8 |
|
|
-8.67 |
32.73 |
|
|
LM powered descent cutoff |
104:29:36 |
|
|
731 |
6,703 |
|
|
|
|
CSM plane change ignition |
169:05:52.14 |
58.6 |
5,349.8 |
|
|
5.60 |
108.83 |
|
|
CSM plane change cutoff |
169:05:59.28 |
58.6 |
5,349.9 |
7.14 |
124 |
5.57 |
108.50 |
64.6 |
55.0 |
LM lunar liftoff ignition |
175:31:47.9 |
|
|
|
|
|
|
|
|
LM lunar ascent orbit cutoff |
175:38:55.7 |
9.9 |
5,523.3 |
427.8 |
6,054.2 |
-9.77 |
5.43 |
40.2 |
7.9 |
LM vernier adjustment |
175:42:18 |
11.2 |
5,515.2 |
|
|
-10.67 |
-5.83 |
|
|
LM terminal phase initiation ignition |
176:26:05 |
40.2 |
5,351.6 |
|
|
6.88 |
-147.37 |
|
|
LM terminal phase initiation cutoff |
176:26:07.5 |
|
|
2.5 |
78.0 |
|
|
|
|
LM terminal phase finalize |
177:08:42 |
|
|
|
|
|
|
64.2 |
40.1 |
CSM/LM docked |
177:41:18 |
65.6 |
5,313.7 |
|
|
-10.53 |
-55.65 |
|
|
LM ascent stage jettisoned |
195:00:12 |
59.2 |
5,347.9 |
|
|
|
|
|
|
CSM separation maneuver |
195:03:13 |
|
|
|
2.0 |
-0.02 |
-115.98 |
|
|
Subsatellite deployed |
196:02:09 |
58.4 |
5,349.4 |
|
|
1.13 |
70.47 |
66 |
52 |