Our
launch database is being revamped into a more user-friendly format.
In the meantime, this simplified version will be provided. |
| Commercial |
Institutional |
Military |
All dates are given in Universal Time (UT).
Back
to 2006
Last modification: July 9, 2007
| January | ||||||||||
| Date |
Site | Launcher | Payload | Country | Mission | Operator | Prime |
Platform |
Mass |
Orbit |
| 10 |
Sriharikota | PSLV-C | CartoSat 2 | India | Remote Sensing | ISRO | ISRO | - | 665
kg |
SSO |
| |
SRE-1 | India | Technology | ISRO | ISRO | - | 615
kg |
SSO |
||
| |
Lapan-Tubsat | Indonesia | Technology | LAPAN | TU
Berlin |
Lapan-Tubsat |
56 kg |
SSO |
||
| |
PehuenSat 1 | Argentina | Technology | AmSat-LU | AmSat-LU |
- |
6 kg |
SSO |
||
| 16 |
Xichang | DF-21 (KT-1?) | [Kill Vehicle #4?] | China | Interception | PLA | n.a. |
- |
n.a. |
Suborbital |
| 18 |
Baykonur | Soyuz U | Progress M-59 | Russia | ISS Cargo | Roskosmos | RKK
Energiya |
7K-TGM |
7,280 kg |
LEO/ISS |
| 30 |
Pacific | Zenit 3SL | NSS-8 | U.S. | Communications | New Skies | Boeing |
BSS-702 |
5,840 kg |
Failure |
| |
|
|||||||||
| February | ||||||||||
| Date |
Site | Launcher | Payload | Country | Mission | Operator | Prime |
Platform |
Mass |
Orbit |
| 02 |
Xichang | CZ-3A | Beidou 2A | China | Navigation | CASC | CAST | DFH-3 |
n.a. |
GTO |
| 07 |
Vandenberg | Minuteman 3 | GT-193GM | U.S. | ICBM | U.S. Air Force | Sandia? |
- |
n.a. |
Suborbital |
| 15 |
Cape Canaveral | Delta 2-7925 | Themis SC1 | U.S. | Science | NASA | Swales | Themis | 125
kg |
HEO |
| |
Themis SC2 | U.S. | Science | NASA | Swales | Themis | 125
kg |
HEO |
||
| |
Themis SC3 | U.S. | Science | NASA | Swales | Themis | 125
kg |
HEO |
||
| |
Themis SC4 | U.S. | Science | NASA | Swales | Themis | 125
kg |
HEO |
||
| |
Themis SC5 | U.S. | Science | NASA | Swales | Themis | 125
kg |
HEO |
||
| 24 |
Tanegashima | H-2A/2024 | IGS-Radar 2 | Japan | Observation | JAXA/CSICE | Melco |
n.a. |
1,200
kg |
SSO |
| |
IGS-Optical 3VS | Japan | Technology | JAXA/CSICE | Melco |
n.a. |
n.a. |
SSO |
||
| |
|
|||||||||
| March | ||||||||||
| Date |
Site | Launcher | Payload | Country | Mission | Operator | Prime |
Platform |
Mass |
Orbit |
| 09 |
Cape Canaveral | Atlas 5/401 | ASTRO | U.S. | Technology | DARPA | Boeing |
- |
600 kg |
LEO |
| |
NextSat/CSC | U.S. | Technology | DARPA | Ball
Aerospace |
RS300 |
400 kg |
LEO |
||
| |
STP-1 | U.S. | Technology | U.S. AFRL | AeroAstro |
- |
170 kg |
LEO |
||
| |
CFE | U.S. | Technology | LANL | SSTL |
MB-80 |
n.a. |
LEO |
||
| |
FalconSat 3 | U.S. | Science | USAFA | USAFA |
- |
50
kg |
LEO |
||
| |
MidStar 1 | U.S. | Technology | USN Postgr. Sch. | USN
Postgr. Sch. |
MIDStar
Mod1 |
n.a. |
LEO |
||
| |
MEPSI-4A? | U.S. | Technology | DARPA | Aerospace
Corp. |
Cubesat |
1 kg |
LEO |
||
| |
MEPSI-4B? | U.S. | Technology | DARPA | Aerospace
Corp. |
Cubesat |
1 kg |
LEO |
||
| 11 |
Kourou | Ariane 5ECA | Skynet 5A | Great-Britain | Communications | Paradigm | EADS
Astrium |
ES-3000 |
4,635 kg |
GTO |
| |
Insat 4B | India | Communications | ISRO | ISRO |
I3K |
3,035 kg |
GTO |
||
| 21 |
Kwajalein | Falcon 1 | DemoSat | U.S. | Technology | DARPA | n.a. |
- |
n.a. |
Failure |
| 21 |
Vandenberg | Minotaur 2 | [SBX Target] | U.S. | Technology | MDA | Sandia? |
- |
n.a. |
Suborbital |
| |
|
|||||||||
| April | ||||||||||
| Date |
Site | Launcher | Payload | Country | Mission | Operator | Prime |
Platform |
Mass |
Orbit |
| 07 |
Baykonur | Soyuz FG | Soyuz TMA-10 | Russia, U.S. | ISS Manned | Roskosmos, NASA | RKK
Energiya |
7K-M |
7,250 kg |
LEO/ISS |
| 09 |
Baykonur | Proton M | Anik F3 | Canada | Communications | Télésat Canada | Astrium |
ES-3000 |
4,640 kg |
GTO |
| 11 |
Taiyuan | CZ-2C | Hai Yang 1B | China | Remote Sensing | CASC | AS-DFH-Sat
Ltd |
CAST968 |
360 kg |
SSO |
| 12 |
Xichang | CZ-3A | Beidou 2B | China | Navigation | CASC | CAST | DFH-3 |
n.a. |
GTO |
| 17 |
Baykonur | Dnepr 1 | Egyptsat 1 | Egypt | Remote Sensing | NARSSS | NPO Yuzhnoye | MS-1TK |
100 kg |
SSO |
| |
Saudisat 3 | Saudi Arabia | Science | RSRI | RSRI | - |
35 kg |
SSO |
||
| |
SaudiComsat 3 |
Saudi Arabia | Communications | RSRI | RSRI | - |
12 kg |
SSO |
||
| |
SaudiComsat 4 |
Saudi Arabia | Communications | RSRI | RSRI | - |
12 kg |
SSO |
||
| |
SaudiComsat 5 |
Saudi Arabia | Communications | RSRI | RSRI | - |
12 kg |
SSO |
||
| |
SaudiComsat 6 |
Saudi Arabia | Communications | RSRI | RSRI | - |
12 kg |
SSO |
||
| |
SaudiComsat 7 |
Saudi Arabia | Communications | RSRI | RSRI | - |
12 kg |
SSO |
||
| |
P-Pod-A | PolySat 4 | U.S. | Technology | Cal Poly | Cal Poly | Cubesat |
1 kg |
SSO |
|
| |
P-Pod-A | CAPE-1 | U.S. | Technology | Un. Louisiana | Un. Louisiana | Cubesat |
1 kg |
SSO |
|
| |
P-Pod-A | PolySat 3 | U.S. | Technology | Cal Poly | Cal Poly | Cubesat |
1 kg |
SSO |
|
| |
P-Pod-B | Libertad 1 | Colombia | Technology | Un. S. Arboleda | Un. S. Arboleda | Cubesat |
1 kg |
SSO |
|
| |
P-Pod-B | AeroCube 2 | U.S. | Technology | AeroSpace Corp. | AeroSpace Corp. | Cubesat |
1 kg |
SSO |
|
| |
P-Pod-B | CSTB-1 | U.S. | Technology | Boeing | Boeing | Cubesat |
1 kg |
SSO |
|
| |
P-Pod-C | MAST | U.S. | Technology | Tethers Unltd | Stanford SSDL | Cubesat
x 3 |
3 kg? |
SSO |
|
| 23 |
Sriharikota | PSLV-CA | AGILE | Italy | Sciences | ASI | Carlo
Gavazzi |
MITA |
352 kg |
LEO |
| |
AAM | India | Technology | ISRO | ISRO | - |
185
kg |
LEO |
||
| 24 |
Wallops | Minotaur 1 | NFIRE | U.S. | Technology | U.S. AFRL | GD
C4 Systems |
SA-200B |
494
kg |
LEO |
| 25 |
Vandenberg | Pegasus XL | AIM | U.S. | Science | NASA, Hampton U. | OSC,
Ball |
RS300 |
195
kg |
SSO |
| |
|
|||||||||
| May | ||||||||||
| Date |
Site | Launcher | Payload | Country | Mission | Operator | Prime |
Platform |
Mass |
Orbit |
| 04 |
Kourou | Ariane 5ECA | Astra 1L | Luxembourg | Communications | SES Astra | Lockheed
Martin |
A2100AX |
4,497.5 kg |
GTO |
| |
Galaxy 17 | U.S. | Communications | Intelsat | Thales Alenia Space |
SB-3000B3 |
4,100 kg |
GTO |
||
| 12 |
Baykonur | Soyuz U | Progress M-60 | Russia | ISS Cargo | Roskosmos | RKK
Energiya |
7K-TGM |
7,280 kg |
LEO/ISS |
| 13 |
Xichang | CZ-3B | NigComSat 1 | Nigeria | Communications | NASRDA | CAST |
DFH-4 |
5,150 kg |
GTO |