TITAN 3A TRANSTAGE R/B, 1001

Orbit data source: Space-Track

TITAN 3A TRANSTAGE R/B, 1001 is space debris in LEO originally from a launch on Thu, 11 Feb 1965 UTC via a TITAN IIIA launch vehicle 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
1001, 1965-008A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Martin Marietta
Mission
Spacecraft
Bus & Motor
TRUSS, Unknown motor
Mass
336 kg wet, 336 kg dry
Launch date (UTC)
1965-02-11 (61 years ago)
Launch vehicle
TITAN IIIA
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 2 Nozzle, 1.6 m
Radar Cross Section
8.643 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 TITAN 3A TRANSTAGE R/B
1 01001U 65008A   25241.97851584  .00000007  00000-0 -20187-3 0  9991
2 01001  32.1465  81.3897 0018348 286.6949  73.1535  9.90722556192594
Epoch: 2025-08-29T23:29Z
TLE epoch observation values (Epoch: 2025-08-29T23:29:03.768Z)
Latitude
-0.00003°
Longitude
110.70455°
Altitude
2,773.276 km
Speed
6.604 km/s
True Right ascension
05h 25m 33s
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
16:00:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,798.737 km
Perigee altitude
2,765.123 km
Semi-major axis
9,160.067 km
Eccentricity
0.00183
Inclination
32.1465°
RAAN
81.3897°
Arg. of periapsis
286.6949°
True anomaly
73.35486°
Mean anomaly
73.1535°
Eccentric anomaly
73.25417°
Mean motion
2.47568 °/min
Orbital period
145.41 mins
BSTAR
-0.00020187
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Other satellites on launch #8 in the year 1965 (1965-02-11 UTC)

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