TITAN 3C TRANSTAGE DEB, 19592

Orbit data source: Space-Track

TITAN 3C TRANSTAGE DEB, 19592 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
19592, 1965-108AA
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1965-12-21 (60 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
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 TITAN 3C TRANSTAGE DEB
1 19592U 65108AA  25240.29435287 -.00000048  00000-0  50809-3 0  9997
2 19592  26.8730 326.0097 6710068  36.7845   0.2669  2.84008502337018
Epoch: 2025-08-28T07:03Z
TLE epoch observation values (Epoch: 2025-08-28T07:03:52.087Z)
Latitude
16.71894°
Longitude
-80.6082°
Altitude
542.237 km
Speed
9.813 km/s
True Right ascension
00h 08m 28s
True Declination
16° 37' 17"
Sunlit
Object was in full shadow 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
15:59:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
28,823.764 km
Perigee altitude
552.527 km
Semi-major axis
21,066.283 km
Eccentricity
0.67101
Inclination
26.873°
RAAN
326.0097°
Arg. of periapsis
36.7845°
True anomaly
1.82809°
Mean anomaly
0.2669°
Eccentric anomaly
0.81121°
Mean motion
0.70984 °/min
Orbital period
507.16 mins
BSTAR
0.00050809
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