TITAN 3C TRANSTAGE DEB, 26050

Orbit data source: Space-Track

TITAN 3C TRANSTAGE DEB, 26050 is space debris in HEO originally from a launch on Tue, 21 Dec 1965 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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Identifier
26050, 1965-108AJ
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1965-12-21 (61 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 TITAN 3C TRANSTAGE DEB
1 26050U 65108AJ  26255.66310795 -.00000027  00000-0  61392-2 0  9993
2 26050  26.2603 195.2085 6607575 325.1358   5.5928  2.69858998268589
Epoch: 2026-09-12T15:54Z
TLE epoch observation values (Epoch: 2026-09-12T15:54:52.526Z)
Latitude
-0.00018°
Longitude
-35.25779°
Altitude
1,567.462 km
Speed
9.057 km/s
True Right ascension
13h 00m 31s
True Declination
0° 00' 01"
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
21:27:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
29,819.843 km
Perigee altitude
1,016.015 km
Semi-major axis
21,796.066 km
Eccentricity
0.66076
Inclination
26.2603°
RAAN
195.2085°
Arg. of periapsis
325.1358°
True anomaly
34.70497°
Mean anomaly
5.5928°
Eccentric anomaly
16.07685°
Mean motion
0.67449 °/min
Orbital period
533.74 mins
BSTAR
0.0061392
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