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CONTOUR (27457)
COSPAR: 2002-034A | Alt Name: Contour
Image
Additional Sources
Launch Details
Launch Date
July 3, 2002
Launch Site
Launch Pad
SLC17A
Launch Vehicle
Delta 7425-9.5
Orbital Elements
NORAD ID
27457
International Designator
2002-034A
Epoch
Wed, 07 Aug 2002 16:59:59 GMT
Apogee
Calculating...
Perigee
Calculating...
Inclination
30.55°
Right Ascension
190.61°
Eccentricity
Calculating...
Argument of Perigee
340.46°
Period
2486.12 min
Mean Motion
0.58 rev/day
Latitude
Calculating...
Longitude
Calculating...
Altitude
Calculating...
Velocity
Calculating...
Polar Plot
3D Visualization
Basic Satellite Info
Name
CONTOUR
Alternative Name
Contour
Type
Payload
Status
Unknown
Owner
NASA/APL
Country
United States
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 27457U 02034A 02218.70833333 +.00000000 +00000-0 +00000-0 0 9997
2 27457 030.5521 190.6101 8915936 340.4630 356.7346 00.57921679000002
Source: Celestrak
Summary
The CONTOUR (Contour) satellite, identified by NORAD CAT ID 27457 and OBJECT ID 2002-034A, is a US-owned spacecraft developed for multiple comet flybys under the ownership of NASA/APL. Launched on July 3, 2002, from SLC17A at AFETR using a Delta 7425-9.5 launch vehicle, CONTOUR has an octagonal cylindrical shape with dimensions of 2 meters in length and diameter, and spans 2 meters. The satellite carries equipment such as CRISP, CFI, CIDA, NGIMS, and is powered by body-mounted solar arrays along with batteries for energy storage. Its dry mass is 355 kg, and the launch mass was 435 kg. CONTOUR's mission is focused on comet exploration through flybys, equipped with an AOCS motor for its attitude control system.
Physical Characteristics
Length
2
Diameter
2
Span
2
Dry Mass
355
Launch Mass
435
Shape
Oct Cyl
Radar Cross Section
3.3062
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
Contour
Purpose
Multiple comet flybys
Mission
Multiple comet flybys
Manufacturer
APL
Life Expectancy
Unknown
Bus
Contour
Configuration
Octagonal body, dust shields
Motor
AOCS
Equipment
CRISP, CFI, CIDA, NGIMS
Power System
Body mounted solar-arrays, batteries
ADCS
Unknown
Transmitter Frequency
Unknown
Map
Next Pass
Azimuth Elevation Time (Local)
Start Azimuth
Max Elevation
Stop Azimuth
Time Until
Pass Duration
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