JASON-3 (41240)

COSPAR: 2016-002A | Alt Name: Jason-3

Image
JASON-3 Satellite Image
Additional Sources
Launch Details

Launch Date

January 17, 2016

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

41240

International Designator

2016-002A

Epoch

Sat, 04 Jul 2026 04:01:39 GMT

Apogee

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Perigee

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Inclination

66.04°

Right Ascension

90.14°

Eccentricity

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Argument of Perigee

271.81°

Period

111.83 min

Mean Motion

12.88 rev/day

Latitude

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Longitude

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Altitude

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Velocity

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Polar Plot
3D Visualization
Basic Satellite Info

Name

JASON-3

Alternative Name

Jason-3

Type

Payload

Status

Partially operational

Owner

CNES/NOAA

Country

France

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 41240U 16002A   26185.16781289 -.00000022  00000-0  15986-3 0  9991
2 41240  66.0418  90.1367 0008289 271.8062  88.2008 12.87623395489437

Source: Celestrak

Summary
JASON-3, also known as Jason-3, is a satellite designed for altimetry and radar missions operated by CNES/NOAA. Launched on January 17, 2016, from Vandenberg Air Force Base (SLC4E) using a Falcon 9 launch vehicle, it has a NORAD catalog ID of 41240 and an object ID of 2016-002A. Equipped with the Proteus Bus, its dimensions are 3.7 meters in length, 1.9 meters in diameter, and spans 9.7 meters. The satellite has a launch mass of 553 kg and a dry mass of 525 kg. Key equipment includes Poseidon-3 (#2), Poseidon-B (#3), AMR, DORIS, NavstarP, LRA, powered by two deployable solar arrays and batteries. Its designed lifetime was 3 years but it reached an operational lifespan of 11 years. The satellite's shape is characterized as a box with two panels and has a radar cross-section of 2.7109 square meters.
Physical Characteristics

Length

3.7

Diameter

1.9

Span

9.7

Dry Mass

525

Launch Mass

553

Shape

Box + 2 Pan

Radar Cross Section

2.7109

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Jason-3

Purpose

Altimetry, Radar

Mission

Altimetry, Radar

Manufacturer

THALES

Life Expectancy

3 years (design); 11 years (reached, #2)

Bus

Proteus

Configuration

Proteus Bus

Motor

AOCS

Equipment

Poseidon-3 (#2), Poseidon-B (#3), AMR, DORIS, NavstarP, LRA

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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