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| Mission type | Technology demonstration |
|---|---|
| Operator | Ecuadorian Civilian Space Agency |
| COSPAR ID | 2013-018B  |
| SATCAT no. | 39151 |
| Website | pegaso |
| Mission duration | Design: 1 year Elapsed: 11 years, 2 months, 16 days |
| Orbits completed | 42,192[1] |
| Spacecraft properties | |
| Spacecraft type | 1U CubeSat |
| Manufacturer | Ecuadorian Civilian Space Agency |
| Launch mass | 1.266 kg (2.79 lb)[2] |
| Dimensions | 10×10×75 cm (3.9×3.9×29.5 in)[3] |
| Power | 107 watts maximum[4] |
| Start of mission | |
| Launch date | 26 April 2013, 04:13 (2013-04-26UTC04:13) UTC |
| Rocket | Long March 2D |
| Launch site | Jiuquan, LA-4/SLS-2 |
| Entered service | 5 May 2013 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Sun-synchronous |
| Semi-major axis | 7,006.53 km (4,353.66 mi) |
| Eccentricity | 0.001754 |
| Perigee altitude | 616.11 km (382.83 mi) |
| Apogee altitude | 640.69 km (398.11 mi) |
| Inclination | 97.9743° |
| Period | 97.28 minutes |
| Mean motion | 14.80 |
| Epoch | 17 February 2021, 12:19:30 UTC[1] |
NEE-01 Pegaso (Spanish pronunciation: [peˈɣaso], "Pegasus") is an Ecuadorian technology demonstration satellite, and Ecuador's first satellite launched to space. Built by the Ecuadorian Civilian Space Agency (EXA), it is a nanosatellite of the single-unit CubeSat class.[5] The spacecraft's instruments include a dual visible and infrared camera which allows the spacecraft to take pictures and transmit live video from space.
After the completion of its HERMES-A ground station in April 2010, EXA authorised the construction of Ecuador's first satellite.[3] A number of restrictions and demands were imposed on the project: EXA was solely responsible for the spacecraft design and technology research, all construction had to take place within Ecuador, the project must be "future-enabling" and result in a technological breakthrough, and its mission must be educational in nature.[4] The completed Pegaso was presented to the public on 4 April 2011.[5] All research and construction of the satellite was performed by Ecuadorian personnel at a cost of US$30,000. Funding for testing and launch services was provided by the Ecuadorian Defense Ministry.[4]
While originally planned to be orbited by a Russian Dnepr, delays with the rocket forced EXA to move the satellite's launch to China.[6] Pegaso was eventually launched as a secondary payload aboard a Chinese Long March 2D from the Jiuquan Satellite Launch Center's SLS Pad 2 on 26 April 2013, 04:13 UTC.[7][8] It was placed into an elliptical orbit around Earth of approximately 600 by 900 kilometres (370 by 560 mi).[9]
The primary objective of Pegaso was to operate in space and transmit spacecraft telemetry for at least one year. In that time, it was intended to test various on-board systems and technologies, as well as serve as an educational tool for grade school students and undergraduates.[4]
The satellite's primary instrument is a 720p HD camera, provided by EarthCam, capable of recording in both visible and infrared light.[3][9] This video, along with telemetry and other data, was broadcast from the spacecraft to the HERMES-A ground station via a three-watt television transmitter.[3] It was meant to allow the public to view live video of the Earth from orbit and give researchers the capability to search for near-Earth objects.[9][10]
To protect against damaging environmental factors, Pegaso employs the Space Environment Attenuation Manifold (SEAM/NEMEA), a multi-layer polymer insulation which is designed to block alpha and beta particles, X-ray and gamma radiation, and up to 67% of incoming heat. The insulation additionally provides the spacecraft some degree of protection against EMP and plasma discharge events, and allows Pegaso to retain heat during orbital night.[11] Further thermal control is obtained with a thin sheet of carbon nanotubes layered over a heat-reflecting surface, which helps to equalise the temperature throughout the vehicle.[4]
The spacecraft's solar panels, at 1.5 millimetres (0.059 in) thick, are among the thinnest ever deployed on a satellite.[9] Pegaso's 57 solar cells are capable of generating 14.25 watts[12] and feed 32 on-board 900 mA·h batteries, producing a maximum of 107 watts available power.[4][13] The solar panel and antenna deployment systems made use of memory metals, passively activated by solar radiation, which allowed for smoother deployment and less agitation of the vehicle's attitude.[4]
For passive attitude control, Pegaso uses a series of magnets and inertial-magnetic dampers for single-axis alignment along Earth's magnetic field.[4]
The satellite operated normally[10] until 23 May 2013; at approximately 05:38 UTC, Pegaso passed very close to the spent upper stage of a 1985 Tsyklon-3 rocket over the Indian Ocean. While there was no direct collision between the satellite and upper stage, Pegaso is believed to have suffered a "glancing blow" after passing through a debris cloud around the Tsyklon stage and striking one of the small pieces.[14][15] After the incident, the satellite was found to be "spinning wildly over two of its axes" and unable to communicate with its ground station.[14] While efforts were made to reestablish control of Pegaso,[15] on 28 August 2013 the decision was made by EXA and the Ecuadorian government to declare the satellite lost.[16]
On 25 January 2014, EXA recovered the audio segment of the Pegaso signal during the first public transmission from NEE-02 Krysaor, verifying that Pegaso had survived its collision with the Tsyklon debris and was operating.[17] EXA announced that it had installed a miniature repeater device aboard Krysaor called PERSEUS, and that this was used to recover the Pegaso signal.[18][19]
Media related to NEE-01 Pegaso at Wikimedia Commons
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| May | Zhongxing 11 |
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Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). | |
