TITAN 3C TRANSTAGE R/B, 3432

Orbit data source: Space-Track

TITAN 3C TRANSTAGE R/B, 3432 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.

Not visible in the next 10 days
Identifier
3432, 1968-081E
Orbit
GEO
Country
Flag of USUS
Related business
Manufacturer
Martin Marietta
Mission
Spacecraft
Bus & Motor
TRANSTAGE, Unknown motor
Mass
~1,950 kg wet, ~1,950 kg dry
Launch date (UTC)
1968-09-26 (57 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 2 Nozzle, 2.3 m
Radar Cross Section
14.974 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 TITAN 3C TRANSTAGE R/B
1 03432U 68081E   25258.96634435 -.00000184  00000-0  00000-0 0  9991
2 03432   1.4316  39.5490 0093594 282.2521 146.3728  1.01517371119201
Epoch: 2025-09-15T23:11Z
TLE epoch observation values (Epoch: 2025-09-15T23:11:32.151Z)
Latitude
1.32527°
Longitude
125.71113°
Altitude
35,767.432 km
Speed
3.063 km/s
True Right ascension
07h 15m 02s
True Declination
1° 19' 26"
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
10:14:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,833.477 km
Perigee altitude
35,050.653 km
Semi-major axis
41,820.202 km
Eccentricity
0.00936
Inclination
1.4316°
RAAN
39.549°
Arg. of periapsis
282.2521°
True anomaly
146.961°
Mean anomaly
146.3728°
Eccentric anomaly
146.66747°
Mean motion
0.25378 °/min
Orbital period
1,418.53 mins
BSTAR
0
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Computing Atmospheric mass density...

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