**DELTA 1 R/B(2) *, 11792**

Orbit data source: Space-Track

DELTA 1 R/B(2) *, 11792 is space debris in HEO originally from a launch on Wed, 26 Oct 1966 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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<iframe src="https://www.satcat.com/sats-embedded/11792?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/11792?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

11792, 1966-096C

Orbit

HEO

Country

Related business

European Space Agency (FR)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-10-26 (59 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: 2 days ago

TLE from 2 days ago

0 DELTA 1 R/B(2) *
1 11792U 66096C   25286.78453439  .00015962  00000-0  13772-1 0  9997
2 11792  17.8074 239.9518 6094407 298.5825  13.7993  3.81539683421921

Epoch: 2025-10-13T18:49Z

TLE epoch observation values (Epoch: 2025-10-13T18:49:43.771Z)

Latitude

-0.00025°

Longitude

-65.12644°

Altitude

2,031.027 km

Speed

8.471 km/s

True Right ascension

15h 59m 33s

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

17:55:07

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

21,472.013 km

Perigee altitude

380.195 km

Semi-major axis

17,304.241 km

Eccentricity

0.60944

Inclination

17.8074°

RAAN

239.9518°

Arg. of periapsis

298.5825°

True anomaly

61.42883°

Mean anomaly

13.7993°

Eccentric anomaly

32.62528°

Mean motion

0.95349 °/min

Orbital period

377.56 mins

BSTAR

0.013772

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Other satellites on launch #96 in the year 1966 (1966-10-26 UTC)

INTELSAT 2-F1, 2514

DELTA 1 R/B(1), 2515 (Decayed)

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DELTA 1 R/B(2) * Visibility forecast

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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.
305 mins	2025-10-16 03:49:39.459Z	253.659° W	2025-10-16 05:52:39.459Z	213.324° SW	39.446°	2025-10-16 08:54:39.459Z	150.942° SSE
54 mins	2025-10-16 22:22:39.459Z	183.781° SSW	2025-10-16 22:41:39.459Z	130.542° SE	27.333°	2025-10-16 23:16:39.459Z	104.117° ESE

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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out DELTA 1 R/B(2) *, 11792 on other resources

View DELTA 1 R/B(2) *, 11792 on Heavens-Above

View DELTA 1 R/B(2) *, 11792 on Keep Track

View DELTA 1 R/B(2) *, 11792 on Celestrak

View DELTA 1 R/B(2) *, 11792 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

DELTA 1 R/B(2) *, 11792

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2025-10-13T18:49:43.771Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #96 in the year 1966 (1966-10-26 UTC)

DELTA 1 R/B(2) * Visibility forecast

Co-orbital & Co-planar RSOs

Check out DELTA 1 R/B(2) *, 11792 on other resources

Documentation

**DELTA 1 R/B(2) *, 11792**

Expand to show TLE details & history
Last TLE update: 2 days ago