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: 2 days ago

TLE from 2 days ago
0 TITAN 4 CENTAUR R/B
1 27169U 02001B   26126.91828075  .00000106  00000-0  00000-0 0  9992
2 27169  10.1115  30.1350 0049108 134.6752 225.6426  1.00193898 25966
Epoch: 2026-05-06T22:02Z
TLE epoch observation values (Epoch: 2026-05-06T22:02:19.456Z)
Latitude
0.00001°
Longitude
-165.29839°
Altitude
35,953.396 km
Speed
3.063 km/s
True Right ascension
02h 00m 13s
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
00:00:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,016.64 km
Perigee altitude
35,602.29 km
Semi-major axis
42,187.602 km
Eccentricity
0.00491
Inclination
10.1115°
RAAN
30.135°
Arg. of periapsis
134.6752°
True anomaly
225.24197°
Mean anomaly
225.6426°
Eccentric anomaly
225.44211°
Mean motion
0.25048 °/min
Orbital period
1,437.26 mins
BSTAR
0
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Other satellites on launch #1 in the year 2002 (2002-01-14 UTC)

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