Main payload Deimos-2, KazEOSat 2 and multiple small satellites launch on June 19 2014 with a Dnepr rocket from Dombarovsky airbase.
Multiple satellite mission aimed at 600 km circular, sun-synchronous orbit with descending node 22:30 local time.
Precise time aimed for: 19:11:11 UTC.
| Name | Description | Information |
| Deimos-2 | Spanish satellite for optical Earth imaging – member of the Disaster Monitoring Constellation, follow-on to Deimos 1 (2009-041A/35681) | Deimos-2 |
| KazEOSat 2 | (Kazcosmos Earth Observation Satellite) – Medium-resolution observation satellite owned by Kazakhstan. Known as DZZ-MR prior to launch. | KazEOSat 2 |
| AprizeSat 9 | Small satellite for data collection from small fixed and mobile ground stations. | |
| AprizeSat 10 | Small satellite for data collection from small fixed and mobile ground stations. | |
| BRITE Montreal | (BRIght Target Explorer) – one of six satellites in a Canadian constellation to make astronomical observations, particularly long-duration observations of bright stars with extremely long periods of oscillation. | BRITE constellation |
| BRITE Toronto | (BRIght Target Explorer) – one of six satellites in a Canadian constellation to make astronomical observations, particularly long-duration observations of bright stars with extremely long periods of oscillation. | BRITE constellation |
| BugSat 1 | (Tita) – technology demonstration mission for a new design earth observation satellite, testing aerials, camera, GPS receiver and a radio system, launch facilitated by ISILaunch – responsible for most of the Cubesats on this Dnepr. | |
| Hodoyoshi-3 | (to be confirmed) small, three axis stabilised satellite for Earth imaging from the University of Tokyo, also carries a store and forward comms payload. | |
| Hodoyoshi-4 | (to be confirmed) small, three axis stabilised satellite for Earth imaging from the University of Tokyo, also carries a store and forward comms payload. | |
| SaudiSat-4 | (to be confirmed) satellite from King Abdulaziz City for Science and Technology (KACST) in Saudi Arabia carrying an experiment jointly designed with NASA Ames Reearch Centre to investigate electrostatic build-up. | |
| Aurora (TabletSat-2U-EO) | Russian technology demonstration satellite with an Earth observation still and video camera system. | Sputnix |
| Unisat 6 | payload includes an amateur radio communications system but its principal task is as a Cubesat dispenser. Inisat 6 will release them 25 hr 34 min after it has separated from the launch vehicle. | |
| AeroCube 6 | 1U Cubesat from Aerospace Corporation in the US, payload undisclosed. | |
| ANTELSat | 2U Cubesat from Uruguay’s Universidad de la República and the government owned ANTEL (Administración Nacional de Telecomunicaciones). It carries developmental communications systems operating at VHF,UHF and S-band, and an Earth-imaging system with detectors in the near infrared and visible bands. | |
| Lemur 1 | 3U Cubesat from Nanosatisfi with a technology demonstration payload of visible and IR imagers. | |
| TIGRISat | 3U Cubesat for detection of desert dust storms over Iraq – built by Iraqi students at La Sapienza University, Rome. | |
| DUCHIFAT | 1U Cubesat buily by secondary school students at the Space Laboratory of the Herzliya Science Centre, Israel with support from the Israeli Amateur Radio Organization, it will transmit real-time information using the Automatic Position Reporting System (APRS) protocol. | |
| DTUSat 2 | 1U Cubesat from the National Space Institute at the Technical University of Denmark to provide a spaceborne radio-tracking system capable of locating birds fitted with transmitters on their migration routes. | |
| Flock 1C-1 – Flock 1C-11 | 3U Cubesat, part of Planet Labs “Flock 1C” consisting of 11 Earth imaging satellites. | |
| NanosatC-Br1 | 1U Cubesat from Brazil’s Southern Regional Space Research Cente, built in collaboration with the Space Science Laboratory of the Federal University of Santa Maria and the Brazilian Space Agency – INPE. | |
| PACE | (Platform for Attitude Control Experiments) – 2U Cubesat developed by students at the National Cheng Kung University (NCKU) in Tainan, Taiwan to verify verify and evaluate varying attitude determination and control strategies. | |
| Perseus-M 1 | 6U (3U x 2U) Cubesat from Dauria Aerospace equipped with a remote sensing imaging system and a receiver for AIS transmissions from ships. | |
| Perseus-M 2 | 6U (3U x 2U) Cubesat from Dauria Aerospace equipped with a remote sensing imaging system and a receiver for AIS transmissions from ships. | |
| PolyITAN | 1U Cubesat from the National Technical University of Ukraine, equipped with a Sun sensor, orientation system and a GLONASS/GPS navigation system. | |
| POPSAT-HIP 1 | 3U Cubesat from Microspace Rapid of Singapore equipped with an imaging system and a cold gas thruster system for attitude control. | |
| QB50p1 | 2U Cubesat, one of a pair of precursor satellites for the QB50 project. Carries an Ion and Neutral Mass Spectrometer to study the Earth’s lower thermosphere. | FUNcube-3 |
| QB50p2 | 2U Cubesat, one of a pair of precursor satellites for the QB50 project. Carries FIPEX (Φ Probe Experiment) to study the presence of atomic Oxygen. |
The Quadpack/slot allocations are as follows (information courtesy of ISIS):
QuadPack-1:
Slot 1 – QB50p1 (2U, Belgium) + NANOSATC-BR1 (1U, Brazil)
Slot 2 – QB50p2 (2U, Belgium) + DTUSAT-2 (1U, Denmark)
Slot 3 – POPSAT-HIP1 (3U, Singapore)
Slot 4 – PACE (2U, Belgium/Taiwan) + DUCHIFAT (1U, Israel)
QuadPack-2:
Slot 1 – 2U Mass Dummy* (not to be deployed) + PolyITAN-1 (1U, Ukraine)
Slot 2 – Flock-1C (3U, US)
Slot 3 – Flock-1C (3U, US)
Slot 4 – Flock-1C (3U, US)
* replaces a 2U Cubesat that was not ready for the preparation cut-off date.
QuadPack-3:
Slot 1 – Flock-1C (3U, US)
Slot 2 – Flock-1C (3U, US)
Slot 3 – Flock-1C (3U, US)
Slot 4 – Flock-1C (3U, US)
QuadPack-4:
Slot 1 – Flock-1C (3U, US)
Slot 2 – Flock-1C (3U, US)
Slot 3 – Flock-1C (3U, US)
Slot 4 – Flock-1C (3U, US)
QuadPack-5:
1 – PERSEUS-M1 (6U – 3U x 2U, US)
2 – PERSEUS-M2 (6U – 3U x 2U, US)
Source: www.zarya.info