**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 (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: 1 week ago

TLE from 1 week ago

0 DELTA 1 R/B(2) *
1 11792U 66096C   26153.00034859  .00001384  00000-0  20535-2 0  9996
2 11792  17.7927  69.4732 6047781 254.2772  34.6959  3.84567679430804

Epoch: 2026-06-02T00:00Z

TLE epoch observation values (Epoch: 2026-06-02T00:00:30.118Z)

Latitude

0.00023°

Longitude

178.82109°

Altitude

6,689.633 km

Speed

6.152 km/s

True Right ascension

04h 37m 42s

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

05:06:10

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

21,245.353 km

Perigee altitude

424.927 km

Semi-major axis

17,213.277 km

Eccentricity

0.60478

Inclination

17.7927°

RAAN

69.4732°

Arg. of periapsis

254.2772°

True anomaly

105.71661°

Mean anomaly

34.6959°

Eccentric anomaly

66.46463°

Mean motion

0.96105 °/min

Orbital period

374.59 mins

BSTAR

0.0020535

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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.
230 mins	2026-06-08 18:57:57.867Z	127.351° SE	2026-06-08 19:11:57.867Z	121.724° SE	31.168°	2026-06-08 22:47:57.867Z	97.558° ESE
273 mins	2026-06-09 01:12:57.867Z	262.256° W	2026-06-09 05:05:57.867Z	232.954° WSW	30.098°	2026-06-09 05:45:57.867Z	169.79° S

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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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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: 1 week ago

TLE from 1 week ago

TLE epoch observation values (Epoch: 2026-06-02T00:00:30.118Z)

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: 1 week ago