TITAN 4 CENTAUR R/B, 27169

Orbit data source: Space-Track

TITAN 4 CENTAUR R/B, 27169 is space debris in GEO originally from a launch on Mon, 14 Jan 2002 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
27169, 2002-001B
Orbit
GEO
Country
Flag of USUS
Related business
Manufacturer
LMA
Mission
Spacecraft
Bus & Motor
CENTAUR T, RL-10 X2
Mass
~1,840 kg wet, ~1,840 kg dry
Launch date (UTC)
2002-01-14 (24 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 4.5 m
Radar Cross Section
37.970 m²

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 TITAN 4 CENTAUR R/B
1 27169U 02001B   25242.32424766 -.00000283  00000-0  00000-0 0  9991
2 27169   9.7312  31.4758 0052150 129.5940 230.9497  1.00167263 23465
Epoch: 2025-08-30T07:46Z
TLE epoch observation values (Epoch: 2025-08-30T07:46:54.997Z)
Latitude
-0.00001°
Longitude
-63.9493°
Altitude
35,955.32 km
Speed
3.063 km/s
True Right ascension
02h 06m 09s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
06:26:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,036.994 km
Perigee altitude
35,596.899 km
Semi-major axis
42,195.084 km
Eccentricity
0.00522
Inclination
9.7312°
RAAN
31.4758°
Arg. of periapsis
129.594°
True anomaly
230.48752°
Mean anomaly
230.9497°
Eccentric anomaly
230.71842°
Mean motion
0.25041 °/min
Orbital period
1,437.65 mins
BSTAR
0
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Other satellites on launch #1 in the year 2002 (2002-01-14 UTC)

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