TITAN 3C TRANSTAGE R/B, 3692

Orbit data source: Space-Track

TITAN 3C TRANSTAGE R/B, 3692 is space debris in GEO originally from a launch on Sun, 09 Feb 1969 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.

Loading next visibility...
Identifier
3692, 1969-013B
Orbit
GEO
Country
Flag of USUS
Related business
Manufacturer
Martin Marietta
Mission
Spacecraft
Bus & Motor
TRANSTAGE, Unknown motor
Mass
2,028 kg wet, 2,028 kg dry
Launch date (UTC)
1969-02-09 (57 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 TITAN 3C TRANSTAGE R/B
1  3692U 69013B   26004.80932766 -.00000237  00000-0  00000+0 0  9994
2  3692   0.8809  76.6900 0166126  36.0092 250.6855  0.97536413 40729
Epoch: 2026-01-04T19:25Z
TLE epoch observation values (Epoch: 2026-01-04T19:25:25.909Z)
Latitude
-0.865°
Longitude
-34.16096°
Altitude
36,817.33 km
Speed
3.029 km/s
True Right ascension
00h 06m 27s
True Declination
0° 51' 51"
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
02:03:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,285.856 km
Perigee altitude
35,858.818 km
Semi-major axis
42,950.474 km
Eccentricity
0.01661
Inclination
0.8809°
RAAN
76.69°
Arg. of periapsis
36.0092°
True anomaly
248.90153°
Mean anomaly
250.6855°
Eccentric anomaly
249.79226°
Mean motion
0.24383 °/min
Orbital period
1,476.42 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|