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: 9 hours ago

TLE from 9 hours ago
0 TITAN 4 CENTAUR R/B
1 27169U 02001B   25299.23254887 -.00000182  00000-0  00000-0 0  9996
2 27169   9.8183  31.1844 0051673 132.0759 228.3139  1.00149083 24039
Epoch: 2025-10-26T05:34Z
TLE epoch observation values (Epoch: 2025-10-26T05:34:52.222Z)
Latitude
0.00001°
Longitude
-87.46335°
Altitude
35,966.863 km
Speed
3.063 km/s
True Right ascension
02h 04m 25s
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
09:44:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,040.113 km
Perigee altitude
35,603.991 km
Semi-major axis
42,200.189 km
Eccentricity
0.00517
Inclination
9.8183°
RAAN
31.1844°
Arg. of periapsis
132.0759°
True anomaly
227.87359°
Mean anomaly
228.3139°
Eccentric anomaly
228.09356°
Mean motion
0.25036 °/min
Orbital period
1,437.91 mins
BSTAR
0
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Other satellites on launch #1 in the year 2002 (2002-01-14 UTC)

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