TITAN 3C TRANSTAGE DEB, 39296
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 39296 is space debris in GEO originally from a launch on Thu, 26 Sep 1968 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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39296 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
23 hours ago
Origin
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & history
TLE from 23 hours ago
0 TITAN 3C TRANSTAGE DEB
1 39296U 68081AG 25199.20902600 .00000091 00000-0 00000-0 0 9997
2 39296 1.2696 5.0939 0155670 330.8609 79.8554 1.00587281 48332Epoch: 2025-07-18T05:00Z
TLE epoch observation values (Epoch: 2025-07-18T05:00:59.846Z)
Latitude
1.01239°
Longitude
46.05688°
Altitude
35,594.942 km
Speed
3.085 km/s
True Right ascension
03h 50m 16s
True Declination
1° 00' 41"
Sunlit
Visualization orbit readout
Latitude
0.75079°
Longitude
29.73398°
Altitude
35,417.853 km
Speed
3.098 km/s
Apparent Right ascension
02h 56m 21s
Apparent Declination
-4° 21' 49"
Sunlit
Visualization observer readout
Local Sidereal Time
16:36:33
Azimuth
39.001° NE
Elevation
-47.873°
Doppler factor
1
Orbital elements
Apogee altitude
36,354.475 km
Perigee altitude
35,044.432 km
Semi-major axis
42,077.59 km
Eccentricity
0.01557
Inclination
1.2696°
RAAN
5.0939°
Arg. of periapsis
330.8609°
True anomaly
81.61712°
Mean anomaly
79.8554°
Eccentric anomaly
80.73569°
Mean motion
0.25146 °/min
Orbital period
1,431.65 mins
BSTAR
0
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Other satellites on launch #81 in the year 1968 (1968-09-26 UTC)
TITAN 3C TRANSTAGE DEB Visibility
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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39296 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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