Space Brief 28 Apr 2025
Today's highlights include SpaceX's 250th Starlink mission, a key Senate vote for NASA's next administrator, and insights into satellite missions and movements.
INTELSAT 902 (IS-902) (26900)
COSPAR: 2001-039A | Alt Name: INTELSAT 902
Image
Additional Sources
Launch Details
Launch Date
August 30, 2001
Launch Site
FRGUI
Launch Pad
ELA2
Launch Vehicle
Ariane 44L
Orbital Elements
NORAD ID
26900
International Designator
2001-039A
Epoch
Wed, 17 Jun 2026 12:43:48 GMT
Apogee
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Perigee
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Inclination
6.12°
Right Ascension
71.78°
Eccentricity
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Argument of Perigee
11.26°
Period
1436.09 min
Mean Motion
1.00 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 902 (IS-902)
Alternative Name
INTELSAT 902
Type
Payload
Status
Operational
Owner
INTELD
Country
United States
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 26900U 01039A 26168.53041905 -.00000291 00000-0 00000+0 0 9992
2 26900 6.1182 71.7793 0004329 11.2555 323.5996 1.00271937 90699
Source: Celestrak
Summary
INTELSAT 902 (IS-902) is a communication satellite launched on August 30, 2001, from ELA2 launch pad at FRGUI using the Ariane 44L launch vehicle. The spacecraft has dimensions of 5.6 meters in length and 2.8 meters in diameter with a span of 31 meters. It was manufactured by LOR based on the SSL-1300HL configuration and is equipped with 44 C-band transponders and 12 Ku-band transponders for communication purposes. The satellite has a dry mass of 1978 kg and a launch mass of 4723 kg, powered by two deployable solar arrays and batteries. Its shape consists of a box structure with two panels and two dishes. INTELSAT 902 is owned by INTELD and operated for a lifetime of approximately 13 years.
Physical Characteristics
Length
5.6
Diameter
2.8
Span
31
Dry Mass
1978
Launch Mass
4723
Shape
Box + 2 Pan + 2 Dish
Radar Cross Section
14.1589
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
INTELSAT 902
Purpose
Communication
Mission
Communication
Manufacturer
LOR
Life Expectancy
13 years
Bus
FS-1300HL
Configuration
SSL-1300HL
Motor
R-4D-11-164
Equipment
44 C-band transponders, 12 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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