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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27169 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast 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
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
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)
TITAN 4 CENTAUR R/B Visibility forecast
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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1440 mins | 2025-08-31 14:46:34.076Z | 118.478° SE | 2025-09-01 13:19:34.076Z | 118.995° SE | 30.558° | 2025-09-01 14:46:34.076Z | 118.863° SE |
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27169 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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