TITAN 3C TRANSTAGE DEB, 1672 (Decayed)
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 1672 was space debris in LEO originally from a launch on Fri, 15 Oct 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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1672 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
0.160 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 TITAN 3C TRANSTAGE DEB
1 1672U 65082AK 24261.96163434 .08108025 19368+0 14883-1 0 9993
2 1672 32.3347 209.3354 0009789 224.3317 135.6591 16.07032588 80144Epoch: 2024-09-17T23:04Z
TLE epoch observation values (Epoch: 2024-09-17T23:04:45.206Z)
Latitude
0.00001°
Longitude
-134.22172°
Altitude
258.226 km
Speed
7.752 km/s
True Right ascension
13h 57m 20s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
19:24:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
265.289 km
Perigee altitude
252.295 km
Semi-major axis
6,636.929 km
Eccentricity
0.00098
Inclination
32.3347°
RAAN
209.3354°
Arg. of periapsis
224.3317°
True anomaly
135.73743°
Mean anomaly
135.6591°
Eccentric anomaly
135.69827°
Mean motion
4.01414 °/min
Orbital period
89.68 mins
BSTAR
0.014883
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Other satellites on launch #82 in the year 1965 (1965-10-15 UTC)
TITAN 3C TRANSTAGE DEB Visibility
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Authenticating...
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