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Information message about launch progress
"Proton-M", "Breeze-M", "Express-AM7"

Document: 11. Total: 12
Create: 19.03.2015 13:36:30 (MDT)


Summary SC launch information

¹

Event of flight cyclogram

Predicted flight time

Data
source

Measuring values

[h:m:s from L-OC]

[s from L-OC]

time [s from L-OC]

deviation [s]

1

Gyroplatform activation end

01:04:54.99

-5.01

Proton-M

-5.01

0.00

2

SE1 ignition

01:04:58.24

-1.76

Proton-M

-1.77

0.01

3

Lift-off contact

01:05:00.00

0.00

Proton-M

0.00

0.00

4

SE2 ignition

01:06:55.38

115.38

Proton-M

114.85

0.53

5

Stage 1-2 separation

01:06:59.63

119.63

Proton-M

119.05

0.58

6

VE3 ignition

01:10:23.78

323.78

Proton-M

324.27

0.49

7

SE2 burnout

01:10:26.48

326.48

Proton-M

326.99

0.51

8

Stage 2-3 separation

01:10:27.18

327.18

Proton-M

327.71

0.53

9

SE3 ignition

01:10:29.58

329.58

Proton-M

330.14

0.56

10

HF jettison

01:10:44.98

344.98

Proton-M

345.47

0.49

11

Fairing jettison indication

01:10:46.88

346.88

Proton-M

345.57

1.31

12

Preliminary command

01:14:30.13

570.13

Proton-M

571.05

0.92

13

Main command

01:14:42.06

582.06

Proton-M

581.57

0.49

14

OU separation

01:14:42.22

582.22

Proton-M

581.70

0.52

15

US ICE 1- ignition

01:16:02.22

662.22

Breeze-M

662.18

0.04

16

US SE 1- ignition

01:16:16.22

676.22

Breeze-M

676.07

0.15

17

US ICE 1- burnout

01:16:18.12

678.12

Breeze-M

677.90

0.22

18

US SE 1- burnout

01:20:46.81

946.81

Breeze-M

943.19

3.62

19

US ICE 2- ignition

02:12:13.00

4033.00

Breeze-M

4033.08

0.08

20

US SE 2- ignition

02:12:33.00

4053.00

Breeze-M

4053.27

0.27

21

US ICE 2- burnout

02:12:34.90

4054.90

Breeze-M

4055.11

0.21

22

US SE 2- burnout

02:30:16.93

5116.93

Breeze-M

5111.02

5.91

23

US ICE 3- ignition

04:32:48.00

12468.00

Breeze-M

12468.36

0.36

24

US SE 3- ignition

04:33:12.00

12492.00

Breeze-M

12492.21

0.21

25

US ICE 3- burnout

04:33:13.90

12493.90

Breeze-M

12494.31

0.41

26

US SE 3- burnout

04:45:34.40

13234.40

Breeze-M

13233.55

0.85

27

US ICE 4- ignition

04:46:18.60

13278.60

Breeze-M

13277.86

0.74

28

APT separation

04:46:24.40

13284.40

Breeze-M

13283.72

0.68

29

US ICE 4- burnout

04:46:26.60

13286.60

Breeze-M

13285.72

0.88

30

US ICE 5- ignition

04:47:43.40

13363.40

Breeze-M

13363.58

0.18

31

US SE 4- ignition

04:47:51.40

13371.40

Breeze-M

13371.70

0.30

32

US ICE 5- burnout

04:47:53.30

13373.30

Breeze-M

13373.54

0.24

33

US SE 4- burnout

04:52:55.59

13675.59

Breeze-M

13672.91

2.68

34

US ICE 6- ignition

09:57:23.00

31943.00

Breeze-M

31943.16

0.16

35

US SE 5- ignition

09:57:33.00

31953.00

Breeze-M

31953.19

0.19

36

US ICE 6- burnout

09:57:34.90

31954.90

Breeze-M

31955.35

0.45

37

US SE 5- burnout

10:04:37.09

32377.09

Breeze-M

32376.36

0.73

38

"Express-AM7" SC separation

10:18:00.00

33180.00

Breeze-M

33170.72

9.28

39

US ICE 7- ignition

12:21:40.00

40600.00

Breeze-M

40600.21

0.21

40

US ICE 7- burnout

12:21:52.00

40612.00

Breeze-M

40612.40

0.40

41

US ICE 8- ignition

13:33:20.00

44900.00

Breeze-M

44900.42

0.42

42

US ICE 8- burnout

13:35:00.00

45000.00

Breeze-M

45000.69

0.69

Used abbreviations:

APT- Additional propellant tank    ETC- Engine thrust control
F- Fuel    GS- Gyro Settings
GTSV- Ground Tracking Stations Visibility
HF- Head fairing    ICE- US impulse correction engine
L-OC- Lift-Off contact    MC- Main command
MDT- Moscow Decree time    ND- Nominal duty
NTL- Nomihal thrust level    O- Oxidant
ODCC- Onboard digital computer complex    OU- Orbital unit
PC- Preliminary command    PU- Propulsion unit
SC- Spacecraft    SHU- Spacehead unit
SE- Sustainer engine    SEU- Sustainer engine unit
StE- Stabilization engine    US- Upper stage
UTC- Universal Coordinated Time    VE- Vernier engine

Sub-orbital trajectory.Final orbit parameter estimation per MBC

MDT of orbit.parameters ( day.month.year hour:min:sec) - 19.03.2015 01:14:42

¹

Parameter

Estimation

Nominal

Deviation

Limit

Comment

1

T [h.m.s]

1:21:16.6

1:21:16.8

0:0:0.1

-----------

-------------------

2

a [km]

6215.44

6215.57

0.12

-----------

-------------------

3

e

0.0536330

0.0535633

0.0000696

-----------

-------------------

4

i

51 °33 '16 "

51 °32 '52 "

0 °0 '24 "

-----------

-------------------

5

Hp [km]

-488.91

-488.36

0.55

-----------

-------------------

6

Ha [km]

177.80

177.49

0.30

-----------

-------------------

Parking orbit.Final orbit parameter estimation per MBC

MDT of orbit.parameters ( day.month.year hour:min:sec) - 19.03.2015 01:20:56

¹

Parameter

Estimation

Nominal

Deviation

Limit

Comment

1

T [h.m.s]

1:27:59.1

1:27:59.2

0:0:0.1

-----------

-------------------

2

a [km]

6552.91

6553.00

0.09

-----------

-------------------

3

e

0.0000254

0.0000001

0.0000253

-----------

-------------------

4

i

51 °33 '33 "

51 °33 '10 "

0 °0 '22 "

-----------

-------------------

5

Hp [km]

181.74

182.00

0.26

-----------

-------------------

6

Ha [km]

182.07

182.00

0.07

-----------

-------------------

Intermediate orbit.Final orbit parameter estimation per MBC

MDT of orbit.parameters ( day.month.year hour:min:sec) - 19.03.2015 02:30:26

¹

Parameter

Estimation

Nominal

Deviation

Limit

Comment

1

T [h.m.s]

2:21:55.0

2:21:55.6

0:0:0.6

-----------

-------------------

2

a [km]

9012.58

9013.00

0.42

-----------

-------------------

3

e

0.2623941

0.2623986

0.0000045

-----------

-------------------

4

i

50 °18 '59 "

50 °17 '60 "

0 °0 '59 "

-----------

-------------------

5

Hp [km]

276.73

277.00

0.27

-----------

-------------------

6

Ha [km]

5006.43

5007.00

0.57

-----------

-------------------

Transfer orbit.Final orbit parameter estimation per MBC

MDT of orbit.parameters ( day.month.year hour:min:sec) - 19.03.2015 04:53:05

¹

Parameter

Estimation

Nominal

Deviation

Limit

Comment

1

T [h.m.s]

10:35:45.1

10:35:55.2

0:0:10.1

-----------

-------------------

2

a [km]

24491.67

24495.98

4.31

-----------

-------------------

3

e

0.7220264

0.7220769

0.0000504

-----------

-------------------

4

i

49 °6 '13 "

49 °6 '0 "

0 °0 '13 "

-----------

-------------------

5

Hp [km]

437.04

437.00

0.04

-----------

-------------------

6

Ha [km]

35804.30

35812.96

8.66

-----------

-------------------

"Express-AM7" target orbit.Final orbit parameter estimation per MBC

MDT of orbit.parameters ( day.month.year hour:min:sec) - 19.03.2015 10:04:47

¹

Parameter

Estimation

Nominal

Deviation

Limit

Comment

1

T [h.m.s]

12:14:17.2

12:14:51.0

0:0:33.8

-----------

-------------------

2

a [km]

26961.07

26974.88

13.80

-----------

-------------------

3

e

0.5634528

0.5630814

0.0003714

-----------

-------------------

4

i

19 °57 '22 "

20 °0 '1 "

0 °2 '38 "

-----------

-------------------

5

Hp [km]

5398.78

5414.83

16.04

-----------

-------------------

6

Ha [km]

35781.36

35792.93

11.56

-----------

-------------------

Used abbreviations and notation:

MBC          - Main Ballistic Center
SDO MEI   - Special Design Office MEI
SSC           - Space Surveillance Center
T               - orbital period
a               - semi-major axis
e               - eccentricity
i                - inclination
Hp             - perigee altitude
Ha             - apogee altitude

Screen shots:

Video
Video
Video
Video
Video
Video
Video
Video
Video
Video
1-st stage separation
First stage impact area
2-nd stage separation
HF jettison
Second stage and HF impact area
US separation
End of booster phase
End of booster phase
End of booster phase
End of booster phase
US main engine action 1-st ign. (ICE)
US main engine action (1-st ign.)
US main engine action (2-nd ign.)
US main engine action (3-rd ign.)
APT separation
US main engine action (4-th ign.)
US main engine action (5-th ign.)
SC separation
SC separation
SC separation
US withdrawel

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