CRYOSAT 2

NORAD 36508· COSPAR 2010-013A· ISS / Science· LEO
Launch
Launched on Apr 8, 2010 from 109/95, Kazakhstan aboard a Dnepr 1.
Dnepr 1 | Cryosat-2
CRYOSAT 2
European Space Agency · CC BY-SA 3.0 igo · via Wikimedia Commons
Live · TLE epoch 2026-07-13 14:46 UTC
Orbit class
LEO — Low Earth Orbit (circular, < 2,000 km)
Operator
European Space Agency
Country
European Space Agency
Manufacturer
Astrium
Launched
Apr 8, 2010
Mass
750 kg
Apogee
725 km
Perigee
722 km
Inclination
92.04°
Period
1.65 h

About CRYOSAT 2

CryoSat-2 is an Earth-observation satellite operated by the European Space Agency (ESA), designed to study changes in the cryosphere — the frozen regions of our planet. Catalogued under NORAD ID 36508 and international designator 2010-013A, it occupies a near-circular low Earth orbit at an altitude of roughly 722–725 km above the surface. Since its launch in April 2010, it has served as one of the most important tools available to scientists studying the behavior and long-term trends of polar ice, contributing data that informs climate research, sea-level projections, and our broader understanding of Earth's changing frozen environments.

Mission and Purpose

The central scientific goal of CryoSat-2 is to precisely measure the thickness of sea ice floating in the Arctic Ocean and to track variations in the mass and elevation of ice sheets, particularly those covering Greenland and Antarctica. This distinction — measuring *thickness* rather than merely surface extent — is critical. Satellite imagery and passive microwave sensors had long been capable of mapping where sea ice exists, but determining how thick that ice is, and therefore how much frozen water it actually represents, demands a fundamentally different approach. CryoSat-2 was purpose-built to close that gap.

The satellite achieves its measurements primarily through radar altimetry. By timing the return of microwave pulses bounced off ice surfaces, the instrument can resolve the height of the ice surface with extraordinary precision, and from that height data, scientists can infer ice thickness by accounting for the density of ice relative to seawater and the fraction of an ice floe that floats below the waterline. Over an extended time series, repeated passes over the same regions allow researchers to detect subtle changes in surface elevation that correspond to ice thinning or thickening — changes that might amount to only a few centimeters per year but carry enormous implications for sea-level rise and polar ecosystems.

Although the Arctic was identified as the mission's primary focus area — particularly the question of whether summer sea ice is undergoing sustained multi-year thinning — CryoSat-2's capabilities extend well beyond the Arctic basin. Data from the satellite have been applied to the Antarctic ice sheet and sea-ice environment, where long-term mass balance questions are equally pressing. Oceanographic applications have also emerged, as the precision altimetry instrument is capable of resolving sea-surface height variations in the open ocean between ice floes, contributing to studies of ocean circulation and mesoscale eddies. This versatility has made CryoSat-2 a wider-purpose Earth observation asset than its original cryospheric mandate might suggest.

It is worth noting the broader programmatic context. CryoSat-2 is part of ESA's Earth Explorer program, a series of research-oriented missions each designed to address a specific gap in scientific understanding of the Earth system. Earth Explorer missions are typically characterized by highly specialized instruments, relatively modest spacecraft sizes, and scientific objectives defined through competitive peer review. CryoSat-2 follows directly from a predecessor mission, CryoSat, which was lost due to a launch vehicle failure in 2005. The decision to rebuild and relaunch the satellite reflected the scientific community's assessment that the measurements it would provide were irreplaceable.

Orbit and Tracking

CryoSat-2 orbits Earth in a low Earth orbit (LEO) that is very nearly circular, with an apogee of 725 km and a perigee of 722 km — a difference of only 3 km, indicating a well-maintained, stable orbit with very little eccentricity. The satellite completes one full orbit every 99.1 minutes, meaning it circles the planet approximately 14 to 15 times per day. Its orbital inclination of 92.0° places it in a slightly retrograde orbit, just past the threshold of a purely polar orbit. This high inclination is not accidental: it allows the satellite to pass over or near both poles on every orbit, providing the coverage of Arctic and Antarctic regions that its scientific mission demands.

A near-polar inclination of this kind is a standard design choice for Earth observation satellites targeting high-latitude science. By sweeping across a broad range of longitudes over the course of a day while the Earth rotates beneath it, CryoSat-2 achieves near-global coverage with particular density at high latitudes, precisely where its instruments are most needed. The orbit is not sun-synchronous — unlike many remote sensing satellites, which are placed in orbits carefully tuned to maintain a fixed local solar time at every overpass — which means that the satellite crosses the same ground track at varying times of day over its repeat cycle. For a radar altimeter mission, this is acceptable; the instrument does not depend on solar illumination in the way an optical camera would.

The orbit has remained stable since launch, and as of the time of writing, CryoSat-2 has not decayed or reentered the atmosphere. At altitudes in the 720 km range, atmospheric drag is extremely low but not entirely absent; station-keeping maneuvers are periodically required to maintain the precise ground-track repeat pattern that scientific data continuity demands.

For satellite trackers, CryoSat-2 passes regularly over most inhabited latitudes, though its relatively small size and non-reflective design make it a challenging naked-eye target compared to larger spacecraft.

Design and Operator

CryoSat-2 was manufactured by Astrium, the European aerospace company that has produced a large number of ESA's science and Earth-observation spacecraft. The satellite has a launch mass of 750 kg, placing it in the medium-small class of scientific satellites — substantial enough to carry a sophisticated radar altimetry package and supporting systems, but modest compared to large operational Earth-observation platforms.

The satellite is owned and operated by the European Space Agency, an intergovernmental organization representing member states across Europe. ESA's Earth Observation Directorate manages the CryoSat-2 mission, overseeing operations from its ground stations and distributing scientific data to the research community. ESA has made CryoSat-2 data openly available to qualified scientific users on a widespread basis, which has contributed to a broad and productive body of published research drawing on the satellite's measurements.

The specific technical configuration of the mission's instruments, onboard systems, and operational details beyond those noted here are outside the scope of what is verifiable from the catalog record for this entry.

Scientific Significance and Current Status

CryoSat-2 has, by any reasonable measure, been a scientifically productive mission. The data it has generated have underpinned numerous peer-reviewed studies addressing the rate of Arctic sea-ice volume decline, the mass balance of the Greenland ice sheet, and changes in Antarctic ice dynamics. These findings have fed directly into major international climate assessments, including successive reports from the Intergovernmental Panel on Climate Change, which rely on observational datasets of precisely the kind CryoSat-2 provides to constrain projections of future sea-level rise.

The satellite launched at a moment when the scientific need for this kind of data was acute. Arctic sea-ice extent had been declining for decades based on passive microwave observations, but the question of whether the remaining ice was also thinning — and if so, at what rate — could not be answered without dedicated thickness measurements. CryoSat-2 was designed to answer that question definitively, and the data record it has accumulated now spans well over a decade, long enough to support robust trend analysis independent of year-to-year variability.

The longevity of the mission has also created challenges and opportunities. Like any spacecraft, CryoSat-2 carries finite consumables and operates systems that age over time. The fact that it remains operational well beyond its original design lifetime represents significant added value to the scientific community. At the same time, the longer the mission continues, the more pressing the question of continuity becomes: ensuring that future satellite missions can extend and calibrate against CryoSat-2's data record is a concern that ESA and the broader cryospheric science community have actively addressed through mission planning for successor instruments.

CryoSat-2 is registered in the satellite catalog as a payload in the LEO orbit class, and as of the current catalog record, it remains in orbit and operational status information is not recorded in the public catalog entry. Its continued presence in orbit is confirmed by ongoing tracking.

How to Spot It

CryoSat-2 is not generally considered an easy naked-eye target. At 750 kg, it is a relatively compact spacecraft without large solar array panels or reflective structures designed to produce bright visual returns. It orbits at an altitude of approximately 722–725 km, which is high enough that passes occur at reasonably predictable intervals, but the satellite's intrinsic brightness is low compared to larger platforms such as the International Space Station or Hubble Space Telescope.

Observers using the orbital data available on this page — inclination 92.0°, period 99.1 minutes, altitude around 723 km — can generate pass predictions for their location using standard tracking tools. The high inclination means that CryoSat-2 passes are visible from virtually all latitudes, including high northern and southern latitudes where the satellite spends proportionally more of its time. Passes near the horizon at twilight, when the spacecraft is sunlit against a darkened sky, offer the best prospects for visual detection with optical aid.

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