·ISRO PSLV-C37 / Planet Labs Flock-3p

15 February 2017: ISRO PSLV-C37 Deploys 104 Satellites on a Single Launch Including 88 Planet Labs 3U ‘Dove’ Imagers & Nayif-1

On 15 February 2017, India’s PSLV-C37 launched from Sriharikota carrying 101 international CubeSats alongside Cartosat-2D, led by 88 3U Planet Dove satellites.

Following the deployment of the first 28 Flock-1 3U CubeSats from the International Space Station in February 2014, Planet Labs scaled 3U nanosatellite manufacturing into an assembly-line industrial process.

On 15 February 2017, the Indian Space Research Organisation’s (ISRO) Polar Satellite Launch Vehicle (PSLV-C37) injected 104 spacecraft into a 505 km Sun-synchronous orbit in under 11 minutes—including 88 3U Dove satellites (Flock-3p) released from ISISPACE QuadPack dispensers and the UAE’s first 1U CubeSat Nayif-1 (EO-88).

Using differential atmospheric drag (alternating between high-drag and low-drag solar array attitudes without onboard propulsion), the 88 3U Dove spacecraft phased themselves into a uniform 'string-of-pearls' ring around the Earth.

CELESTRAK SATCAT & TELEMETRY RECORD

Verified Spacecraft Key Facts & Orbital Dossier

SpacecraftClassOperator / CountryLaunch & VehicleNORAD / COSPAROrbit & RF DownlinkCatalog Status
Nayif-1 (EO-88)
1U
MBRSC / American University of Sharjah
AE
PSLV-XL (PSLV-C37) · ISIPOD
NORAD 42017
2017-008BX
145.94 MHz (VHF/UHF)
Decayed
Flock-1 / Dove (SuperDove)
3U
Planet Labs
US
Antares 120 (Cygnus CRS-1 / ISS) · Nanoracks NRCSD
Unassigned
UHF / S / X
Completed

Catalogued Mission Summaries & Flight Notes

Nayif-1 (EO-88) (1U, 2017):
First CubeSat of the United Arab Emirates (1U, 1.1 kg), launched on the record 104-satellite PSLV-C37 mission with an active magnetorquer/sun-sensor ADCS and FUNcube U/V transponder; operated for over six years before re-entering on 18 July 2023.
Flock-1 / Dove (SuperDove) (3U, 2014):
Operational 3U Earth-observation CubeSat bus (~5 kg) with deployable solar wings, 3-axis reaction wheel + star tracker ADCS, 90 mm Maksutov telescope (3–5 m GSD), and high-speed X-band downlink.

Related SatWiki Specifications & Fleet Records

Related Historical Dossiers from This Era