TITAN 3A DEB (TRUSS), 1000

Orbit data source: Space-Track

TITAN 3A DEB (TRUSS), 1000 is space debris in LEO originally from a launch on Thu, 11 Feb 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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ISO8601 Format

Identifier

1000, 1965-008B

Orbit

LEO

Last TLE update

15 hours ago

Origin

United States Space Force (US)

Manufacturer

Martin Marietta

Mission

Spacecraft

Bus & Motor

TRANSTAGE, Unknown motor

Mass

1,950 kg wet, 1,950 kg dry

Launch date (UTC)

1965-02-11 (60 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 2 Nozzle, 2.3 m

Radar Cross Section

14.974 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 15 hours ago

0 TITAN 3A DEB (TRUSS)
1 01000U 65008B   25221.62101326  .00000008  00000-0  58138-5 0  9991
2 01000  32.1498 354.7157 0012201 329.4347  30.5439  9.88890761186511

Epoch: 2025-08-09T14:54Z

TLE epoch observation values (Epoch: 2025-08-09T14:54:15.545Z)

Latitude

-0.00001°

Longitude

172.79682°

Altitude

2,779.793 km

Speed

6.603 km/s

True Right ascension

23h 38m 51s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

31.77019°

Longitude

-87.56545°

Altitude

2,797.577 km

Speed

6.593 km/s

Apparent Right ascension

07h 05m 21s

Apparent Declination

3° 27' 32"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

20:22:40

Azimuth

26.918° NE

Elevation

-43.136°

Doppler factor

Orbital elements

Apogee altitude

2,804.421 km

Perigee altitude

2,782.041 km

Semi-major axis

9,171.368 km

Eccentricity

0.00122

Inclination

32.1498°

RAAN

354.7157°

Arg. of periapsis

329.4347°

True anomaly

30.61505°

Mean anomaly

30.5439°

Eccentric anomaly

30.57946°

Mean motion

2.47111 °/min

Orbital period

145.68 mins

BSTAR

0.0000058138

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Other satellites on launch #8 in the year 1965 (1965-02-11 UTC)

TITAN 3A TRANSTAGE R/B, 1001

LES 1, 1002

TITAN 3A DEB (TRUSS) Visibility forecast

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.
23 mins	2025-08-10 10:22:13.925Z	193.837° SSW	2025-08-10 10:34:13.925Z	141.055° SSE	25.317°	2025-08-10 10:45:13.925Z	94.19° ESE
29 mins	2025-08-10 12:56:13.925Z	234.06° WSW	2025-08-10 13:10:13.925Z	164.394° S	39.702°	2025-08-10 13:25:13.925Z	90.513° ESE
29 mins	2025-08-10 15:34:13.925Z	260.53° W	2025-08-10 15:48:13.925Z	182.834° SSW	42.119°	2025-08-10 16:03:13.925Z	108.736° ESE
27 mins	2025-08-10 18:12:13.925Z	269.839° W	2025-08-10 18:25:13.925Z	208.275° SW	34.932°	2025-08-10 18:39:13.925Z	142.003° SSE
14 mins	2025-08-10 20:55:13.925Z	248.338° W	2025-08-10 21:01:13.925Z	224.192° SW	15.479°	2025-08-10 21:09:13.925Z	192.306° SSW

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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Check out TITAN 3A DEB (TRUSS), 1000 on other resources

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View TITAN 3A DEB (TRUSS), 1000 on Keep Track

View TITAN 3A DEB (TRUSS), 1000 on Celestrak

View TITAN 3A DEB (TRUSS), 1000 on Gunter's Space Page

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