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Information message about launch progress
"Proton-M", "Breeze-M", "Sirius FM6"

Document: 11. Total: 12
Create: 26.10.2013 09:39:41 (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

21:08:49.00

-5.00

Proton-M

-5.00

0.00

2

SE1 ignition

21:08:52.25

-1.75

Proton-M

-1.76

0.01

3

Lift-off contact

21:08:54.00

0.00

Proton-M

0.00

0.00

4

SE2 ignition

21:10:49.38

115.38

Proton-M

114.70

0.68

5

Stage 1-2 separation

21:10:53.63

119.63

Proton-M

119.78

0.15

6

VE3 ignition

21:14:17.78

323.78

Proton-M

324.06

0.28

7

SE2 burnout

21:14:20.48

326.48

Proton-M

326.78

0.30

8

Stage 2-3 separation

21:14:21.18

327.18

Proton-M

327.50

0.32

9

SE3 ignition

21:14:23.58

329.58

Proton-M

329.92

0.34

10

HF jettison

21:14:38.98

344.98

Proton-M

345.26

0.28

11

Fairing jettison indication

21:14:40.88

346.88

Proton-M

345.36

1.52

12

Preliminary command

21:18:24.13

570.13

Proton-M

570.31

0.18

13

Main command

21:18:36.06

582.06

Proton-M

581.32

0.74

14

OU separation

21:18:36.22

582.22

Proton-M

581.45

0.77

15

US ICE 1- ignition

21:20:26.22

692.22

Breeze-M

692.03

0.19

16

US SE 1- ignition

21:20:40.22

706.22

Breeze-M

705.92

0.30

17

US ICE 1- burnout

21:20:42.12

708.12

Breeze-M

707.76

0.36

18

US SE 1- burnout

21:25:06.95

972.95

Breeze-M

965.18

7.77

19

US ICE 2- ignition

22:16:07.00

4033.00

Breeze-M

4033.18

0.18

20

US SE 2- ignition

22:16:27.00

4053.00

Breeze-M

4053.24

0.24

21

US ICE 2- burnout

22:16:28.90

4054.90

Breeze-M

4055.33

0.43

22

US SE 2- burnout

22:34:12.85

5118.85

Breeze-M

5092.11

26.74

23

US ICE 3- ignition

00:36:49.00

12475.00

Breeze-M

12475.14

0.14

24

US SE 3- ignition

00:37:13.00

12499.00

Breeze-M

12499.19

0.19

25

US ICE 3- burnout

00:37:14.90

12500.90

Breeze-M

12501.09

0.19

26

US SE 3- burnout

00:48:41.64

13187.64

Breeze-M

13176.37

11.27

27

US ICE 4- ignition

00:49:25.84

13231.84

Breeze-M

13220.68

11.16

28

APT separation

00:49:31.64

13237.64

Breeze-M

13226.54

11.10

29

US ICE 4- burnout

00:49:33.84

13239.84

Breeze-M

13228.54

11.30

30

US ICE 5- ignition

00:50:50.64

13316.64

No date

31

US SE 4- ignition

00:50:58.64

13324.64

Breeze-M

13324.88

0.24

32

US ICE 5- burnout

00:51:00.54

13326.54

Breeze-M

13326.84

0.30

33

US SE 4- burnout

00:56:53.59

13679.59

Breeze-M

13670.25

9.34

34

US ICE 6- ignition

06:00:48.00

31914.00

Breeze-M

31914.16

0.16

35

US SE 5- ignition

06:00:58.00

31924.00

Breeze-M

31924.39

0.39

36

US ICE 6- burnout

06:00:59.90

31925.90

Breeze-M

31926.22

0.32

37

US SE 5- burnout

06:07:10.82

32296.82

Breeze-M

32289.82

7.00

38

"Sirius FM6" SC separation

06:20:14.00

33080.00

Breeze-M

33065.30

14.70

39

US ICE 7- ignition

08:25:34.00

40600.00

Breeze-M

40600.11

0.11

40

US ICE 7- burnout

08:25:46.00

40612.00

Ball center

40612.36

0.36

41

US ICE 8- ignition

09:33:34.00

44680.00

Breeze-M

44680.32

0.32

42

US ICE 8- burnout

09:35:14.00

44780.00

Breeze-M

44780.45

0.45

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) - 25.10.2013 21:18:36

¹

Parameter

Estimation

Nominal

Deviation

Limit

Comment

1

T [h.m.s]

1:21:7.0

1:21:16.8

0:0:9.7

-----------

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

2

a [km]

6207.29

6215.57

8.28

-----------

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

3

e

0.0555390

0.0535623

0.0019767

-----------

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

4

i

51 °32 '54 "

51 °32 '52 "

0 °0 '1 "

-----------

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

5

Hp [km]

-515.59

-495.48

20.11

-----------

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

6

Ha [km]

173.90

170.36

3.54

-----------

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

Parking orbit.Final orbit parameter estimation per MBC

MDT of orbit.parameters ( day.month.year hour:min:sec) - 25.10.2013 21:25:16

¹

Parameter

Estimation

Nominal

Deviation

Limit

Comment

1

T [h.m.s]

1:27:56.6

1:27:56.8

0:0:0.3

-----------

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

2

a [km]

6550.78

6551.00

0.22

-----------

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

3

e

0.0000201

0.0000001

0.0000200

-----------

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

4

i

51 °33 '7 "

51 °33 '13 "

0 °0 '7 "

-----------

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

5

Hp [km]

172.51

172.86

0.35

-----------

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

6

Ha [km]

172.77

172.86

0.09

-----------

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

Intermediate orbit.Final orbit parameter estimation per MBC

MDT of orbit.parameters ( day.month.year hour:min:sec) - 25.10.2013 22:34:22

¹

Parameter

Estimation

Nominal

Deviation

Limit

Comment

1

T [h.m.s]

2:21:54.9

2:21:55.6

0:0:0.7

-----------

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

2

a [km]

9012.49

9013.00

0.51

-----------

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

3

e

0.2623946

0.2623988

0.0000042

-----------

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

4

i

50 °19 '53 "

50 °18 '0 "

0 °1 '53 "

-----------

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

5

Hp [km]

269.52

269.86

0.34

-----------

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

6

Ha [km]

4999.18

4999.86

0.69

-----------

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

Transfer orbit.Final orbit parameter estimation per MBC

MDT of orbit.parameters ( day.month.year hour:min:sec) - 26.10.2013 00:57:03

¹

Parameter

Estimation

Nominal

Deviation

Limit

Comment

1

T [h.m.s]

10:36:1.3

10:35:52.8

0:0:8.5

-----------

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

2

a [km]

24498.62

24494.98

3.64

-----------

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

3

e

0.7221182

0.7220655

0.0000527

-----------

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

4

i

49 °7 '16 "

49 °6 '0 "

0 °1 '16 "

-----------

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

5

Hp [km]

429.58

429.86

0.28

-----------

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

6

Ha [km]

35811.39

35803.83

7.55

-----------

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

"Sirius FM6" target orbit.Final orbit parameter estimation per MBC

MDT of orbit.parameters ( day.month.year hour:min:sec) - 26.10.2013 06:07:20

¹

Parameter

Estimation

Nominal

Deviation

Limit

Comment

1

T [h.m.s]

11:48:20.3

11:48:50.0

0:0:29.7

-----------

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

2

a [km]

26322.10

26334.36

12.25

-----------

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

3

e

0.6020310

0.6011020

0.0009290

-----------

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

4

i

23 °9 '17 "

23 °11 '1 "

0 °1 '44 "

-----------

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

5

Hp [km]

4097.24

4126.59

29.34

-----------

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

6

Ha [km]

35790.69

35785.86

4.83

-----------

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

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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