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INTELSAT 26 (IS-26) (24732)
COSPAR: 1997-007A | Alt Name: JCSAT R
Image
Additional Sources
Launch Details
Launch Date
February 17, 1997
Launch Site
Launch Pad
LC36B
Launch Vehicle
Atlas IIAS
Orbital Elements
NORAD ID
24732
International Designator
1997-007A
Epoch
Sat, 04 Jul 2026 05:26:24 GMT
Apogee
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Perigee
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Inclination
12.30°
Right Ascension
29.40°
Eccentricity
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Argument of Perigee
292.71°
Period
1455.90 min
Mean Motion
0.99 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
INTELSAT 26 (IS-26)
Alternative Name
JCSAT R
Type
Payload
Status
Non-operational
Owner
JSAT
Country
Japan
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 24732U 97007A 26185.22667737 -.00000073 00000-0 00000-0 0 9994
2 24732 12.3048 29.3994 0009102 292.7092 64.2798 0.98907955107216
Source: Celestrak
Summary
INTELSAT 26 (IS-26), also known as JCSAT R, is a communication satellite operated by JSAT. It was launched on February 17, 1997, from Cape Canaveral Air Force Station's LC36B using an Atlas IIAS launch vehicle. The spacecraft has dimensions of 4 meters in length and 2.8 meters in diameter with a span of 26.2 meters when its solar arrays are deployed. It has a dry mass of 1,600 kilograms and was launched with a total mass of 3,090 kilograms. Equipped with 12 C-band transponders and 28 Ku-band transponders for communication purposes, the satellite is powered by two deployable solar arrays and batteries. The spacecraft design follows the HS-601 bus configuration manufactured by HSES. Its primary mission lasted for about 12 years.
Physical Characteristics
Length
4
Diameter
2.8
Span
26.2
Dry Mass
1600
Launch Mass
3090
Shape
Box + 2 Pan
Radar Cross Section
25.1486
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
JCSAT 4
Purpose
Communication
Mission
Communication
Manufacturer
HSES
Life Expectancy
12 years
Bus
HS-601
Configuration
HS-601
Motor
R-4D-11-300
Equipment
12 C-band transponders, 28 Ku-band transponders
Power System
2 deployable 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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