**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 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

Cyl, 0.8 m

Radar Cross Section

0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago

0 DELTA 1 R/B(2) *
1 11792U 66096C   25242.66408577  .00024010  00000-0  17401-1 0  9996
2 11792  17.8495 272.3661 6116053 238.4460  47.7456  3.79614618420242

Epoch: 2025-08-30T15:56Z

TLE epoch observation values (Epoch: 2025-08-30T15:56:17.01Z)

Latitude

-0.00005°

Longitude

54.1871°

Altitude

9,592.602 km

Speed

5.192 km/s

True Right ascension

18h 09m 24s

True Declination

0° 00' 00"

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

01:32:17

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

21,603.662 km

Perigee altitude

365.439 km

Semi-major axis

17,362.688 km

Eccentricity

0.61161

Inclination

17.8495°

RAAN

272.3661°

Arg. of periapsis

238.446°

True anomaly

121.5103°

Mean anomaly

47.7456°

Eccentric anomaly

82.48719°

Mean motion

0.94868 °/min

Orbital period

379.48 mins

BSTAR

0.017401

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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)

DELTA 1 R/B(2) * Visibility forecast

Observer location: undefined°, undefined°
Set Observer location

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.
212 mins	2025-08-31 23:31:25.611Z	123.637° SE	2025-09-01 01:43:25.611Z	92.987° ESE	14.168°	2025-09-01 03:03:25.611Z	87.038° E
236 mins	2025-09-01 05:57:25.611Z	241.08° WSW	2025-09-01 09:53:25.611Z	218.704° SW	38.728°	2025-09-01 09:53:25.611Z	218.704° SW

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 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: 18 hours ago

TLE from 18 hours ago

TLE epoch observation values (Epoch: 2025-08-30T15:56:17.01Z)

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: 18 hours ago